Apparatus for launching subcaliber projectiles at propellant operating pressures including the range of pressures that may be supplied by human breath

ABSTRACT

An apparatus for efficiently and accurately launching subcaliber projectiles comprises:
         an elongate barrel;   an associated discarding sabot; and   an associated subcaliber projectile.       

     In one embodiment, the sabot includes a registration means adapted to limit lateral displacement of the projectile while simultaneously permitting the projectile to touch the inner surface of the bore of the barrel. An alternative embodiment includes a magnetically attractable portion incorporated into the projectile and a magnetic detent for holding the projectile within the barrel bore in readiness for launching. Other alternative embodiments are disclosed.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No.12/018,802, filed 2008 Jan. 24 by the present inventor, now pending,which claims the benefit of provisional patent application U.S. Ser. No.60/886,295 filed 2007 Jan. 23 by the present inventor, and the benefitof provisional patent application U.S. Ser. No. 60/886,320 filed 2007Jan. 24 by the present inventor. Each patent application identifiedabove is incorporated here by reference in its entirety, as if set forthat length, to provide continuity of disclosure.

FEDERALLY SPONSORED RESEARCH

Not Applicable

SEQUENCE LISTING OR PROGRAM

Not Applicable

BACKGROUND Field of Invention

This invention relates to mechanical guns and projectors, specificallyto such guns and projectors in which fluid pressure is provided by theuser's mouth or lungs. This invention also relates generally to a sabotprojectile; more particularly, a sabot projectile suited for use even atlow operating pressures such as those provided by human breath.

INTRODUCTION

The inventive apparatus and method for launching subcaliber projectilesis adapted to perform efficiently and smoothly at propellant operatingpressures that include the range of pressures that may be supplied bythe breath of a human user. Furthermore, in certain embodiments thediscarding of the associated sabot means features a very quick, cleanseparation from the subcaliber projectile, with sabot discarding fullyoperational at projectile velocities that include the range ofvelocities attainable by projectiles launched by the breath of a humanuser from a blowgun. Thus the instant invention is especiallywell-suited for providing a blowgun which can utilize the breath of theuser to efficiently and accurately launch subcaliber projectiles.

Before moving further into this disclosure, it should be noted that theterm, full caliber, when used herein to refer to blowgun projectiles,may be understood to mean, essentially full caliber, or, substantiallyfull caliber, in order to include the many examples of full caliberblowgun projectiles met with in practical usage which have an actualcaliber or diameter which is slightly less than the caliber of thebarrel bore, in order that the widest portion of the projectile maysubstantially slidingly seal with the barrel bore to prevent excessiveleakage of pressurized air or breath during launch, yet slide throughthe bore without excessive friction or snugness of fit, in order toachieve efficient propulsion. Thus a broadening of the meaning of theterm, full caliber, to be inclusive of all three possibilities ofprojectiles with actual caliber dimension equal to, slightly greaterthan, or slightly less than the caliber dimension of the barrel bore,applies to the fullness of this disclosure, and will be understood toalso apply to information set forth herein concerning the dimensions offull caliber sabot means employed with subcaliber blowgun projectiles.

It will be seen that the instant invention makes possible, in certainembodiments, appropriately low levels of launching resistance of theassociated sabot projectile assembly, and appropriately low or very lowlevels of discarding resistance of the associated sabot means, therebymaking the efficient and accurate launching of subcaliber projectilescompatible with the relatively low operating pressures provided by ahuman user's breath, and with the relatively modest velocities andenergies typically attained by blowgun projectiles accelerated by theuser's breath.

PRIOR ART

Blowguns work in a known manner to utilize the user's breath toaccelerate and launch a projectile. Blowgun performance may be improvedby increasing accuracy, power, and range, which is generallyaccomplished by broad strategies such as increasing launch force orvelocity of the projectile, or by modifying the balance characteristicsand aerodynamic properties of the projectile. Other broad strategies forimproving blowgun performance include providing increased ease ofaiming, as with a sighting mechanism, and providing a blowgun which canfunction as a multi-shot repeater, with the convenience and increasedrate of fire compensating in a certain measure for any deficiencies ofaccuracy or power.

The prior state of the art regarding blowguns and improvements to theirperformance may be generally established by the following cited patents:U.S. Pats. No. 186,651 to Luther C. White and No. 856,813 to JohnSchultz utilized tapered bores with cooperating compressible dartpistons to provide increased launch force. U.S. Pat. No. 344,915 toLewis H. Lang & John W. Hart utilized an interior annular shoulderdetent in cooperation with a compressible dart piston so as to impose atemporary acceleration delay to boost launch force. U.S. Pat. No.4,419,978 to Loftus utilized a pultruded barrel construction tofacilitate proportioning of the bore for a longer power stroke toincrease launch velocity. U.S. Pat. No. 6,588,413 to Yoichi Nagasueutilized an offset mouthpiece to allow sighting alignment of one eyedirectly along the blowgun barrel instead of the typical offsetalignment of the eye when the barrel is aligned directly with the user'smouth. Taking a different approach, U.S. Pat. No. 4,565,009 to Porterutilized a stereoscopic blowgun sighting apparatus which exploits theuser's binocular vision to create an illusionistic overlay image forsuperimposed sighting alignment with the target, suitable for use with abarrel aligned directly with the mouth. U.S. Pat. No. 3,137,287 to RufoD. De Arbun and U.S. Pat. No. 3,124,119 to Carl Ayala provided repeatingblowguns that launched elongate projectiles. U.S. Pat. No. 2,888,003 toSwanson and U.S. Pat. No. 5,850,826 to Guthrie provided repeaterblowguns with tubular magazines that launched spherical projectiles.U.S. Pat. No. 5,544,642 to Guthrie provided a revolver-type repeaterblowgun that selectively launched spherical or elongate projectiles.

The above cited patents are generally relevant to the prior state of theart. The following patents are more specifically related, each havingpartial relevance to one or more aspects of the inventive blowgun. U.S.Pat. No. 873,628 to Charles E. Stivers utilized a conical paper dartpiston for improved bore sealing properties. U.S. Pat. No. 4,283,061 toRolf W. Jordan utilized a dart in which the tapered shaft and lightweight of the hollow impeller piston yield a forwardly disposed centerof gravity to promote aerodynamic stability of the projectile. Perhapsclosest to the instant invention are the immediately following fourblowgun-related patents: U.S. Pat. No. 3,735,748 to Gaylord utilized ablowgun having a plurality of magnets to hold darts on the barrel foreasy access, with one magnet also holding a dart partially loaded withinthe barrel bore. U.S. Pat. No. 2,679,838 to Thompson utilized aprojectile retaining blowgun which may be considered to include a typeof projectile detent. U.S. Pat. No. 4,103,893 to Walker provided atranquilizer dart especially suited for a blowgun, designed for launchwith a sabot described implicitly in the method of use. U.S. Pat. No.632,838 to Jacobs provided a blowgun that launched subcaliber sphericalshot from a blowgun via a full caliber projectile carrier that wasretained in the blowgun bore after launch. However, unlike the instantinvention, none of these patents described or contemplated embodimentsor alternative embodiments which utilized an external magnetic detent orother type of external detent means to assist in locating one or moreelements of a sabot projectile assembly within the blowgun bore pendinglaunch acceleration.

U.S. Pat. No. 3,735,748 to Gaylord may be considered to use a type ofprojectile detent, a magnet mounted near the mouthpiece which may serveto hold a dart partially loaded within the barrel bore. However, it isclearly the intention that the detent should only hold the dart in placewithin the bore in a partially loaded position, rather than in a fullyloaded position. Furthermore, Gaylord does not disclose or contemplatealternative embodiments or methods of use in which such a projectiledetent is used to help locate elements of a sabot projectile assemblywithin the bore and in spatial relation to one another.

U.S. Pat. No. 2,679,838 to Thompson provided a projectile retainingblowgun in the form of a peashooter with a hole in the barrel forpartial insertion of the user's fingertip, which together with aninterior annular shoulder provided by the mouthpiece, may be consideredto function as a type of projectile detent with elements that cooperatein mutual opposition to locate or confine a full caliber projectilewithin the bore prior to launch and to prevent premature projectiledisplacement toward the breech or toward the muzzle. However, likeGaylord, Thompson does not disclose alternative embodiments or methodsof use in which such a projectile detent is used to locate one or moreelements of a sabot projectile assembly. Furthermore, Thompson's type offingertip detent, although an elegant solution for the peashooter andprojectile he discloses, would not be generally applicable to a widevariety of types of blowgun projectiles, particularly certain types ofsabot projectiles that include subcaliber projectiles.

Although U.S. Pat. No. 4,103,893, to Walker does not recite orillustrate a sabot as a numbered element, a sabot is implicit in thedisclosed method of use, which mentions launching the disclosed dartwith a cotton or fibrous pellet inserted into the bore behind the loadeddart. However, Walker makes no provision for a detent to preventpremature sliding of the dart within the bore. Nor would thetranquilizer dart described by Walker exploit the full possibilities ofsubstantial caliber reduction to provide a projectile with sufficientlyhigh sectional density to confer substantial trajectory advantages forlong range application. Instead, Walker's principle intention inincluding a sabot in the method of use seems to be to ensure adequatebore seal of the projectile. The type of cotton pellet sabot described,according to the specified method of use, would not function compatiblywith very substantially reduced-caliber projectiles, particularly oneswithout affixed, substantially full caliber fins to form an interface toprevent blow-past of the sabot around or alongside the subprojectile. Nomention is made of alternative embodiments which would employ sabots ofreduced parasitic mass and friction and greater structural anddimensional uniformity. Nor are disclosed alternative embodiments to thetranquilizer dart suitable for general sporting applications includingtarget shooting and hunting.

U.S. Pat. No. 632,838 to Jacobs does utilize round-shot projectileswhich may be used at a substantial caliber reduction of shot-caliberrelative bore-caliber. Spherical shot or pellets may exhibit highersectional densities than are typical of many elongate full caliberfixed-piston blowgun projectiles. Even so, a spherical projectile,particularly in small shot-caliber sizes, is well recognized as havinglow sectional densities compared to equally calibered elongatesolid-body ammunition. However, Jacobs does not disclose any way to usehis blowgun to launch elongate subcaliber projectiles which could bemore effectively adapted to exhibit high sectional densities in-flight.Instead, Jacob's principle intention is to exploit the convenience andeconomy of shot as a replacement for possibly more complex and expensiveelongate projectiles such as darts. However, if small caliber shot suchas BB shot were launched as full caliber projectiles, thecorrespondingly small barrel bore would excessively restrict the inflowof the user's breath. On the other hand, at larger caliber sizes, fullcaliber metal shot would generally be excessively massive for thrustprovided by a user's breath. Thus, in order to utilize shot as aprojectile source, Jacobs' blowgun exploits increased thrust-to-massratio by launching shot in an oversized bore with a full calibercarrier. However, the shot-retention lip and self-centering cavity ofthe carrier disclosed by Jacobs would not work effectively with elongateprojectiles. The carrier's shot-retention lip may be considered as atype of projectile detent. Jacobs does not describe or contemplate anyalternative detent means, such as an exterior magnetic detent, to holdthe projectile in loaded disposition against the carrier, an arrangementwhich would allow the shot-retention lip to be eliminated and the cavityto be much smaller and shallower, thus facilitating the reduction ofparasitic mass and bearing friction of the carrier. Such an arrangementwould also eliminate the self-centering seating movement of theprojectile within the carrier at launch initiation, thereby minimizingpotential for vibration. Jacobs does not disclose any provision forengaging shot asymmetrically against the carrier, or for letting theshot-projectile ride directly on the bore, arrangements which wouldoffer the possibility of requiring lessened carrier function, so thatthe nominal carrier might instead function primarily as a pusher plug,thereby offering additional opportunity to reduce the parasitic mass andfriction of the carrier or pusher plug. Jacobs also does not discloseany provision to provide the bore with an interior guidance groove toapply enhanced guidance to the shot-projectile or other projectileduring launch. Jacobs discloses a ported barrel and a cushioned stop todecelerate and retain the carrier at the completion of its power stroke.However, Jacobs does not describe or contemplate embodiments in whichprovision is made to engage and decelerate the carrier with a stop meansor catching means that is not only yieldingly cushioned, but is alsoactually structurally displaceable relative the bore, in order to reducepotential of damage to the carrier and blowgun by exploitingconservation of momentum and inelastic collision to reduce the mutualimpact shock of the carrier and the carrier stop upon each other. In theblowgun disclosed by Jacobs, the porting holes or slots needed toactuate partial carrier deceleration before reaching the carrier stopcauses a shortening of the available power stroke length for a givenbore length. Jacobs makes no provision for alternate embodiments inwhich the carrier may be replaced by, or embodied as, a launchablediscarding sabot which is not retained in the bore after launch, thusnot requiring in-bore deceleration, and therefore being able to exploitthe longest possible power stroke for a given bore length to reachmaximum launch velocity. Furthermore, such a discarding sabot might bemore lightly structured than the retainable carrier disclosed by Jacobs,again facilitating reduction of parasitic mass and launch friction.Jacobs also discloses no provision for using bore rifling withpre-formed cooperating carrier surfaces to spin the carrier whenlaunching spherical shot or other projectiles and thereby transferringstabilizing spin to the subprojectile.

Sabots generally work in a known manner to launch subcaliberprojectiles, effectually decreasing the sectional density of aprojectile during launch to achieve higher thrust-to-mass ratio, and bythereafter discarding, restoring a higher level of sectional density tothe projectile for in-flight ballistic advantages and possible terminalballistic advantages.

To achieve efficient and accurate launching of subcaliber projectiles,parasitic mass and bearing friction of the sabot must be kept withinacceptable levels for available thrust. Suitable means must be utilizedso that various other sources of resistance to launching, sabotdisengagement, and sabot discarding are simultaneously limited toacceptable levels compatible with available thrust. Such means muststill ensure secure locating of sabot projectile assembly componentswithin the blowgun after loading, pending launch and during handling.Furthermore, to advantageously obtain higher efficiencies in terms ofballistic advantages, in-flight sectional density of the projectile mustbe made sufficiently high. The applicant knows of no prior-art blowgunable to simultaneously achieve or deliver all of these objects oradvantages.

Prior-art blowguns were unable to efficiently launch subcaliberprojectiles, and were therefore limited to effective use with fullcaliber projectiles. Full caliber projectiles, in order to be propelledby the relatively low operating pressures typically provided by a humanuser's breath, are required to have relatively low sectional densities,since a full caliber projectile with excessively high sectional densitywould be excessively massive for the available thrust and would thus beaccelerated too slowly, achieving low exit velocities, poortrajectories, and probably causing discomfort or strain to the user'sairways and lungs. The low sectional density and correspondingly lowballistic coefficients of full caliber blowgun projectiles means thattheir trajectories are excessively curved, particularly at extendedranges, making maximum range limited and causing targeting compensationat extended ranges to be very difficult due to the large amount ofbarrel elevation needed to compensate for the excessive amount ofvertical drop of the projectile. Using full-caliber projectiles oflighter mass to achieve higher velocities and flattened trajectories mayyield improved performance at close ranges, but at extended rangestrajectory will still be excessively curved, since lightening the massbut keeping the caliber constant results in even lower sectionaldensity.

Another problem encountered with full caliber blowgun projectiles is asevere limitation in the ability to adjust projectile properties such asform factor, mass distribution, and configuration of aerodynamicsurfaces, in order to improve aerodynamic performance and balance toyield benefits such as reduced drag, reduced sensitivity to cross-winds,increased ballistic coefficient, and improved stability and accuracy.This severe limitation is imposed by the requirement that some fixedportion of the projectile must be suitably shaped and sized to serve asa substantially full caliber piston slidingly sealable with the bore ofthe blowgun barrel.

Due to the problems set forth above, prior-art blowguns achieved onlylimited performance. Inadequate ability to improve projectiles in termsof characteristics such as sectional density, form factor, ballisticcoefficient, mass distribution, balance, configuration of aerodynamicsurfaces, and internal ballistic stability caused significant reductionof the benefits that were intended to be provided by prior-art attemptsto improve performance. For example, prior-art strategies that yieldedincreased projectile velocity were able to provide flatter trajectoriesat short ranges, and modest increases in maximum range. However, thefact that full caliber projectiles still often had surprisingly lowsectional densities and correspondingly poor ballistic coefficientsmeant that projectile velocity decreased very rapidly in flight, withthe result that maximum range remained limited, and trajectories,particularly at extended ranges, remained excessively curved, so thatlong range targeting compensation was still very difficult due toexcessive vertical drop of the projectile, while other problems includedtendencies towards balance- and aerodynamic-related instability, alongwith various sources of inconsistency in the orientation and motion ofthe projectile as it was launched into flight. Additionally, the aboveproblems with prior-art blowguns and projectiles tended to encouragemethods of use which did not sufficiently customize blow-guns andprojectiles for each particular user's abilities, skills, and shootingobjectives.

The problems discussed above would seem to make the blowgun a naturalcandidate for application of the solution or strategy of usingsubcaliber projectiles with associated sabot means. Subcaliberprojectiles with associated discarding sabot means, which may also bereferred to as sabot projectiles, have long been employed in varioustypes of artillery and firearms, and provide greatly increased abilityto adjust projectile properties such as form factor and mass, in orderto obtain advantages such as, for example, higher thrust-to-mass ratioduring launch acceleration, as well as improved sectional density andballistic coefficient of the subcaliber projectile as it travels alongits external trajectory. Such advantages in turn can provide performanceimprovements such as increased launch velocity, increased retention ofvelocity and energy downrange, reduced drag, flatter trajectory,increased maximum range, and more efficient target penetration.

However, despite the advantages described above, sabot projectilesolutions have not been effectively employed in prior-art blowguns, dueto the fact that prior-art sabot projectiles are not adapted to belaunched efficiently within the range of operating pressures that may betypically provided by human breath. Furthermore, discarding of prior-artsabots does not operate efficiently within the range of velocitiestypically attainable by blowgun projectiles. Rather, successfulprior-art sabot projectiles are generally designed to be used infirearms, artillery, and the like, in which the propellants employed tolaunch projectiles typically generate operating pressures which aremeasured in hundreds or thousands of pounds per square inch. The verytight fit between a sabot and a barrel bore necessary to form anadequate gas seal against such extremely high pressures of expandingpropellant gases imposes very high levels of launching resistance as thesabot projectile assembly is pushed along the bore during launch.Furthermore, in firearms and artillery, projectile muzzle velocitiestypically approach or exceed the speed of sound, with correspondinglyhigh levels of atmospheric drag encountered by the projectile. Suchextremely high levels of operating pressures and in-flight drag aresufficient to overcome the high levels of launching resistance anddiscarding resistance imposed by the various types of connections orconnecting means used in firearms and artillery for the purpose ofsecuring sabot projectile components together and in correct positionwithin the bore or firing chamber during various stages of the loadingand launching sequence, while maintaining an adequate gas seal.

Sabots utilized in artillery are often somewhat structurally complex,especially if the subprojectile has a very substantial caliber reductionrelative the bore caliber. Such sabots may have a carrier portionstructurally separate from a pusher plug base portion. Some suchcarriers are one-piece, often with slots or other weakening zones tocause fracture into segments or pieces in a predictable manner uponlaunch. Such one-piece carriers are often formed by casting, using thesubprojectile as a core in a casting mold, as in U.S. Pat. No. 4,360,954to Burns et al. Other carriers may be multi-piece, often formed asseveral separate segments. Direct connections, or various types ofintermediary connecting means, are employed to connect base to carrier,carrier segments to one another (where appropriate), and base andcarrier to the subprojectile. Examples of such intermediary connectingmeans include frangible petals and severable spinner bands, as utilizedrespectively in U.S. Pats. No. 4,841,867 and 4,296,687 to Garrett. Inorder to disengage direct connections or intermediary connecting meansbetween the sabot components and the subprojectile, artilleryapplications exploit high levels of inertial, compressive, andcentrifugal forces, and of gas or air pressure loads, to causeobturation, upset, and other structural deformation, rupture, orfracture. For example, U.S. Pat. No. 5,297,492 to Buc utilizespropellant gas pressure entrapped in an internal aft cavity of the sabotto blow apart a solid obturator ring upon muzzle exit, while U.S. Pat.No. 4,735,148 to Holtman et al. exploits high air resistance pressure ofin-flight drag and centrifugal forces generated by a projectile spinrate of approximately 45,000 rpm to shed and disintegrate a plasticcomposite sabot. In a related field, U.S. Pat. No. 5,239,930 to Adams etal. launched a hypervelocity subprojectile with a sabot that included afoam matrix projectile-retaining means, with the foam matrix crumblinginto a powder under the immense linear acceleration forces of launch andthereby disengaging the sabot from the projectile. Forces generatedduring launch in artillery and hypervelocity projector applications aresufficient to overcome high levels of launching and discardingresistance of sabot projectiles. Even in the artillery sabot projectileadapted for launch from a smooth bore in U.S. Pat. No. 5,359,938 toCampoli et al, high operating pressures and high velocities are requiredto overcome high levels of launching, disengaging, and discardingresistance and to actuate the disclosed parallel lift separation method.

Such high levels of launching resistance and discarding resistance arenot able to be overcome efficiently, if at all, by the much loweroperating pressures provided by human breath, and by the considerablylower velocities and energies attainable by blowgun projectiles launchedby human breath. Small arms sabot projectiles typically have a much lesspronounced caliber reduction and are generally less complex thanexamples found in artillery applications. Small arms firearms typicallyemploy sleeve or cup type sabots. Modified cup type sabots for smallarms are often monolithic structures of molded plastic with multipleflexible petal segments extending from a pusher plug base. Such sabotsoften retain the subprojectile in place with a frictional fit,force-fit, interference fit or encapsulation. U.S. Pat. No. 6,073,560 toStone utilized a small arms petalled sabot suitable for muzzle-loadersand other firearms, in which the weighted protions of the petalsassisted in better exploiting centrifugal forces to open the sabot andexpose greater area to air drag.

It may also be noted that some sabot projectiles used in firearms andartillery are able to exploit centrifugal force, produced by spinimparted by barrel rifling, in order to enhance the sabot's performancein peeling away from the projectile quickly and cleanly. However, it isproblematic to apply barrel rifling to blowguns without excessivelyincreasing launching resistance. Also, blowgun rifling would typicallylaunch projectiles with slower spin rates than those imparted to firearmprojectiles, yielding relatively low levels of centrifugal force to beexploited to aid discarding.

An example of a small arms sabot that did not rely on centrifugal forceis U.S. Pat. No. 4,434,718 to Kopsch et al., which utilized a sabotprojectile that included a sabot and finned subcaliber projectilesuitable for launch from a shotgun cartridge through and from a smoothbore barrel. The sabot is a simple, cylindrical shell or can type, withlong thin petals designed to be opened by air pressure. The finnedsubprojectile has fins offset to produce aerodynamically inducedstabilizing spin. It is not explicitly stated how the subprojectile isdispositioned when loaded within the cylindrical sabot other than thatthe backs of the fins are supported on the transverse metal disk.However, taking into consideration the accompanying drawingillustrations, it appears that the intention is for the fins to fitsnugly against the petals when the sabot is loaded within the shotguncartridge case, holding the sabot body in an essentially centeredposition axisymmetric with the sabot cylinder. Certainly that seems theonly method that would not require additional complexity, or extra mass.The crimped forward end of the cartridge shell serves as an additionalor alternative projectile retaining means prior to launch. Stone's sabotprojectile cited above does not require a cartridge shell when used in amuzzle-loader.

It may be useful to summarize several situations likely to result ifprior-art sabot projectiles were used or superficially adapted for usein a blowgun, even relatively simple small arms types such as those inthe above cited U.S. Pats. No. 4,434,718 and No. 6,073,560. First,inadequate operating pressures to overcome launch resistance wouldresult in the sabot projectile either being stuck in the barrel bore, orelse exiting the barrel bore with reduced velocity. Second, in the eventthe sabot projectile did attain satisfactory exit velocity, sincesatisfactory velocities for blowgun projectiles are still typically toolow to actuate discarding of prior-art sabots, there would likely be afailure of the sabot to achieve separation and thereby discard, in whichcase the sabot means and the subcaliber projectile would continue totravel along an external trajectory together, performing in effect as afull caliber projectile and causing the subcaliber projectile to fail toachieve its true function. Even if separation occurred, release wouldlikely not be quick and clean, thus transmitting excessive drag from thesabot means to the subcaliber projectile during discarding, therebylowering projectile velocity, or introducing trajectory inaccuracies forthe projectile, or both. Third, even if the degree of discardingresistance were lowered sufficiently to guarantee successful, cleandiscarding of the sabot means, the consequent looseness or tenuousnessof the connection between the sabot means and the projectile properwould almost certainly result in premature separation of the sabotprojectile components prior to launch acceleration or prior to exit fromthe barrel bore. This summary also indicates a list of pitfalls thatshould preferably be avoided by a successful solution to providing ablowgun that can efficiently and accurately launch subcaliberprojectiles.

It will be apparent to one familiar with the art that even theairgun-compatible sabot utilized in U.S. Pat. No. 5,150,909 to Fitzwaterwould not operate successfully or efficiently at pressures provided byhuman breath. Nor would the sabots utilized in U.S. Pats. No. 422,347 toHyde and 3,536,054 to Stephens et al., even though they are designed foruse in vacuum cannons, which operate at modest pressure differentials.Blowgun pressure differentials, however, are generally even more modest,probably never or rarely exceeding 4 pounds per square inch (psi), with2 psi and lower being much more typical for the average user.

One other blowgun-related patent to be considered is U.S. Pat. No.4,854,294 to Lala, which disclosed a pressure-assisted blowgun in whichthere was no direct connection between the mouthpiece and the blowguntube; rather a breath operated valve was used to connect a source ofpressurized gas at 120 psi to the blowgun tube to launch target darts of10 to 15 grains. Although nominally a blowgun, Lala's apparatus does notutilize the user's breath to propel the projectile, but merely toactuate a pressure valve connected to an external pressure source. Sucha solution may not appeal to those blowgun users who prefer to use theirown breath to provide the motive force to accelerate and launch theprojectile, rather than rely on an external motive source such as acanister of pressurized gas. It may also be appreciated that 10 to 15grain target darts, which are typical masses for commercial wire roddarts used with popular 40 caliber and 50 caliber blowguns, would havevery low sectional densities, even lower than that of a steel BB shotused in mechanical airguns. Lala does not disclose, describe, orcontemplate any alternative embodiments capable of launching subcaliberprojectiles.

It should be emphasized how important it is, in certain embodiments,that when the sabot projectile assembly has completed exiting the borethrough the muzzle opening of the blowgun barrel, and the propulsivethrust has consequently substantially dissipated, there shouldpreferably at that time be, as nearly as possible, substantially nopositive connection between the subcaliber projectile and the sabotmeans, either directly or via intermediary connecting means, as wouldprovide any substantial resistance to axial displacement of thesubcaliber projectile forwardly relative the sabot means, nor to axialdisplacement of the sabot means rearwardly relative the subcaliberprojectile. This point is very important, because at the relatively lowvelocities and energies which blowgun projectiles typically attain, itmay be surprisingly difficult to obtain separation, or clean separation,of the sabot from the subcaliber projectile if there is even a seeminglytenuous connection between the two components which would excessivelyresist the type of relative axial displacement described in thepreceding sentence. Thus, there is the potential for even a seeminglyweak force-fit engagement, frictional engagement, or the like, to beable to either cause failure of the sabot to separate at all or elsecause sabot separation to either be too slow or too violent, therebytransmitting drag or trajectory inaccuracies or both to the projectileproper.

It is therefore adviseable to minimize or eliminate the need forpositive connectios or connecting means between sabot projectileelements by, for example, utilizing some type of external detent such asa magnetic detent. As was seen, closely related blowgun patents did notutilize a detent to locate elements of a sabot projectile in dispositionpending launch. A number of patents in other fields utilize magneticmeans to retain a projectile in loaded desposition pending launch.Examples include U.S. Pat. Nos. 3,463,136 to Vadas et al., 3,142,294 toBaldwin, and 2,293,957 to Wells, all of which disclosed mechanical airguns that utilized a magnetic bolt or magnetic breech pin to hold a BBshot or other magnetically attactable full caliber airgun projectile inloaded position pending launch pressurization. U.S. Pat. No. 4,860,719to Scheiterlein utilized a magnetic hold-down device for holding anarrow securely on the arrowrest of a crossbow without direct contact ofthe hold-down device with the arrow or arrowhead. However, none of thesepatents disclose alternate embodiments or methods of use in which such amagnetic bolt, breech pin, or hold-down device is used to locate anelement of a sabot projectile assembly preparatory to firing; and inparticular to hold a subcaliber projectile in place against, within, orin front of a sabot means in loaded disposition pending launch.

It is also important to note that, despite the seemingly superadequateoperating pressures and projectile velocities available to overcomelaunching resistance and to actuate sabot discarding in firearms andartillery, a survey of certain prior art designs of firearm andartillery sabot projectiles reveals concerns for minimizing adverseeffects on projectile trajectory and accuracy that may be caused duringsabot discarding. For example, U.S. Pat. No. 5,481,980 to Engel et alutilized special parting plane geometry to avoid impact of edges of thesabot segments upon the projectile during sabot separation. U.S. Pat.No. 4,841,867 to Garrett used a sabot base free of direct positivecoupling to the subprojectile so as to provide a more compatibleinterface of the base with the gun barrel. If such concerns forproviding cleaner sabot release and separation are deemed worthy ofattention in adapting sabot projectiles for use in firearms orartillery, they may be considered as even more critical in obtainingoptimal, or even satisfactory, performance from a sabot projectileadapted for use in a blowgun.

Another limiting factor in the performance of prior art blowguns is thatinsufficient correctional guidance is applied to certain portions of theprojectile during launch acceleration, resulting in internal ballisticinstability that translates into accuracy dispersions in theprojectile's external trajectory. Certain prior art designs attempted toaddress this problem, but the means employed resulted in increasedlaunch resistance, increased projectile mass, and undesirableaerodynamic and balance characteristics of the projectile. This may beseen in the cylindrical bodied darts utilized in U.S. Pat. No. 3,735,748to Gaylord, in which the cylindrical piston bodies are intended to alignthe dart, including the forwardly extending rod, coincident with thelongitudinal axis of the barrel bore. However, many typical commercialblowgun darts do not utilize a cylindrical piston body, but rather apiston body that is essentially conical, and which usually does notmaintain the longitudinal axis of the dart in alignment with thelongitudinal axis of the barrel bore. In a typical full caliber blowgunprojectile, the forward end or tip of the projectile, which is often theforward tip of a slender rod, is usually the only point of directcontact between the bore and the often relatively rigid rod, since therod typically angles down from a point of substantially rigid attachmentwith, or insertion into, a full caliber fixed piston, to rest upon thebore. Since the forward tip of the rod is usually the rod's only directpoint of contact with the bore, the rod is provided with only a verysmall area of direct support contact with the bore, and thus veryminimal guidance is applied to the forward end of the rod, which is alsothe forward end of the projectile. This arrangement, in conjunction withthe typically slightly loose fit of the piston within the bore, usuallynecessary in a blowgun projectile to avoid excessive friction andlaunching resistance, leaves some play in the orientation of the dart.Particularly, the forward tip of the rod may slide transversely upon thebore and swing toward the left or right, or possibly even oscillatebetween left and right. The forward tip of the rod may also lift off thebore, due to play of the piston under launch pressure, or due to barrelcurvature, such as that caused by gravity-induced sag, in which casesubstantially no guidance is applied to the forward end of the rodunless contact with the bore is reestablished essentially byhappenstance.

Prior art blowguns also presented certain disadvantages concerned withtarget shooting. Prior art practices for shooting blowgun projectiles attargets and retrieving projectiles from the targets suffered from anexcessively high potential for damage to projectiles, which aretypically intended to be reusable, and from excessive amounts of timeand effort spent in retrieving projectiles from the target after a roundof shooting. Prior art practices also placed limitations on accuracy ofassessment of shot placement on the target face, and made it difficultto practice more than a rather narrow variety of target practiceshooting styles and formats.

Prior art blowguns also presented problems in launching sphericalprojectiles, and certain other essentially non-elongate projectiles,since full caliber spherical projectiles typically had relatively highsectional densities and poor air seal performance, resulting in poorlaunch acceleration and reduced velocities.

SUMMARY

In accordance with one embodiment a blowgun apparatus comprises ablowgun with an associated subcaliber projectile and an associated sabotmeans and an optional mouthpiece. In accordance with another embodimenta blowgun apparatus comprises a blowgun with a detent means with anassociated subcaliber projectile and an associated sabot means and anoptional mouthpiece. In accordance with another embodiment a blowgunapparatus comprises a blowgun with an interiorly disposed projectileguidance means and an optional projectile means.

DRAWINGS Figures

FIG. 1 depicts a side view of the inventive blowgun in an embodimentwhich comprises blowgun 110 with associated subcaliber projectile 140and associated sabot means 170.

FIG. 2 depicts a perspective view of blowgun 110.

FIG. 3 is a side view of foreshaft 150 by itself.

FIG. 4 is a portion of the side view depicted in FIG. 1, enlarged toshow with greater clarity and detail a side view of subcaliberprojectile 140 and sabot means 170.

FIGS. 5 and 6 are, respectively, exploded and assembled perspectiveviews of subcaliber projectile 140.

FIG. 7 and FIG. 8 depict, respectively, exploded and assembledperspective views of sabot projectile assembly 190.

FIG. 9 and FIG. 10 depict, respectively, side elevational and frontelevational views of sabot projectile assembly 190.

FIG. 11 depicts a sectional side view, along section line 11-11 fromFIG. 10, of sabot projectile assembly 190

FIG. 12 depicts a sectional view, on a somewhat enlarged scale forclarity, of sabot projectile assembly 90 along section line 12-12 fromFIG. 9.

FIG. 13 depicts a sectional view, on a somewhat enlarged scale forclarity, of sabot projectile assembly 190 along section line 13-13 fromFIG. 9.

FIG. 14 depicts a perspective view of a possible method by which theuser may manually hold subcaliber projectile 140 and sabot 170 engagedtogether as sabot projectile assembly 190

FIGS. 15 and 16 depict stages in a possible method of loading sabotprojectile assembly 190 into barrel bore 120-4 of blowgun 110.

FIGS. 17 and 18 depict sabot projectile assembly 190 in loaded positionwithin bore 120-4 after completion of loading insertion into and throughbreech 120-2 and before initiation of launch acceleration.

FIG. 19 shows sabot projectile assembly 190 partially displaced alongbore 120-4, traveling under launch acceleration through bore 120-4.

FIG. 20 depicts a perspective view of the distal portion of barrel 120,with the portion at and near muzzle 120-6 partially cut away to showsabot projectile assembly 190 partially exited through and out muzzle120-6.

FIG. 21 is a perspective view depicting discarding separation of sabot170 from subcaliber projectile 140 after sabot 170 has completed exitingthrough and out muzzle 120-6.

FIG. 22 is a side view of the inventive blowgun in another embodimentwhich comprises blowgun 110, associated subcaliber projectile 140, andassociated sabot means 170.

FIG. 23 depicts a perspective view of blowgun 110

FIG. 24 is a side view of foreshaft 150 shown by itself.

FIG. 25 is a portion of the side view depicted in FIG. 22, enlarged toshow with greater clarity and detail a side view of subcaliberprojectile 140 and sabot means 170.

FIGS. 26 and 27 are, respectively, exploded and assembled perspectiveviews of subcaliber projectile 140.

FIG. 28 and FIG. 29 depict, respectively, exploded and assembledperspective views of sabot projectile assembly 190.

FIG. 30 and FIG. 31 depict, respectively, side elevational and frontelevational views of sabot projectile assembly 190.

FIG. 32 depicts a sectional side view of sabot projectile assembly 190,along section line 32-32 from FIG. 31

FIG. 33 depicts a sectional view, on a somewhat enlarged scale forincreased clarity of detail, of sabot projectile assembly 190, alongsection line 33-33 from FIG. 30.

FIG. 34 depicts a sectional view, on a somewhat enlarged scale forincreased clarity of detail, of sabot projectile assembly 190 alongsection line 34-34 from FIG. 30.

FIG. 35 depicts a perspective view of a possible method by which theuser may manually hold subcaliber projectile 140 and sabot 170 engagedtogether as sabot projectile assembly 190

FIG. 36 and FIG. 37 depict stages in a possible method of loading sabotprojectile assembly 190 into barrel bore 120-4 of blowgun 110.

FIGS. 38 and 39 depicted side views of sabot projectile assembly 190confined in fully loaded position by the mutual opposition or mutualconfinement imposed by projectile detent means 210 and sabot detentmeans 220.

FIG. 40 is a sectional view along section line 40-40 from FIG. 39,showing sabot 170 rearwardly engaged by sabot detent means 220.

FIG. 41 shows sabot projectile assembly 190 partially displaced alongbore 120-4, traveling under launch acceleration through bore 120-4

FIG. 42 depicts a perspective view of a distal portion of barrel 120,with the portion at and near muzzle 120-6 partially cut away to showsabot projectile assembly 190 partially exited through and out muzzle120-6.

FIG. 43 is a perspective view depicting discarding separation of sabot170 from subcaliber projectile 140 after sabot 170 has completed exitingthrough and out muzzle 120-6.

FIGS. 44-46 depict another embodiment of the inventive blowgun chosenfor detailed description

FIG. 44 is a side elevation view of blowgun 110 with subcaliberprojectile 140 and sabot means 170 in loaded position within blowgun110.

FIG. 45 is a perspective view of subcaliber projectile 140 and sabotmeans 170.

FIG. 46 shows an exploded perspective view of blowgun 110, withprojectile 140 and sabot 170.

FIGS. 47-51 depict an embodiment of the inventive blowgun whichcomprises blowgun 110 and optional full caliber projectile 600.

FIG. 47 is a perspective view of blowgun 110, partially cut away at andnear breech 120-2 and mouthpiece 130 to show optional projectile 600 inloaded position within bore 120-4 near breech 120-2 and inner surface ofbore 120-4 provided with guidance means 500.

FIGS. 48 and 49 are, respectively, assembled and exploded perspectiveviews of optional full caliber projectile 600.

FIG. 50 is a side elevational view of blowgun 110 with optionalprojectile 600 loaded inside bore 120-4 near breech 120-2, with thecooperating portion of projectile 600 resting in and engaged with groove500.

FIG. 51 is a sectional view along section line 51-51 from FIG. 50,somewhat enlarged to show in greater detail and clarity the cooperatingportion of projectile 600 resting in and engaged with groove 500, andthe cross-sectional shape of groove 500.

REFERENCE NUMERALS

-   -   110 blowgun    -   120 elongate barrel of blowgun    -   120-2 breech opening of bore of blowgun barrel    -   120-3 breech end of blowgun    -   120-4 bore of blowgun barrel    -   120-6 muzzle opening of bore of blowgun barrel    -   120-8 outer surface of blowgun barrel    -   130 optional mouthpiece of blowgun    -   140 subcaliber projectile means    -   150 foreshaft of subcaliber projectile    -   150-2 forward (in use) portion of subcaliber projectile    -   150-3 shoulder defined by transition between forward portion and        rearward portion of subcaliber projectile    -   150-4 rearward (in use) portion of subcaliber projectile    -   160 shaft of subcaliber projectile    -   160-2 forward (in use) opening of shaft of projectile    -   160-3 forward (in use) end of shaft of projectile    -   160-4 rearward (in use) opening of shaft of projectile    -   160-5 rearward (in use) end of shaft of projectile    -   170 sabot means    -   170-2 base of sabot    -   170-4 tip or end opposite base of sabot    -   170-6 forward facing (in use) surface of sabot    -   170-8 rearward facing (in use) surface of sabot    -   190 sabot projectile assembly including sabot and subcaliber        projectile    -   200 detent means    -   210 projectile detent    -   220 sabot detent    -   300 (arrows) breath of user    -   310 (curved arrows) dispersing thrust    -   320 (sharply bent arrows) atmospheric drag    -   500 guidance means in or on surface of bore    -   600 optional full caliber projectile    -   610 full caliber piston means of full caliber projectile    -   620 shaft of full caliber projectile    -   630 foreshaft of full caliber projectile

DETAILED DESCRIPTIONS FIGS. 1-51—Certain Embodiments and Methods ofOperation

Proportions and relative proportions, in the following figures depictingvarious embodiments of my blowgun, are exemplary and are not restrictiveof the invention; however, in embodiments depicted and in certain otherembodiments as well, sabot means 170 is preferably, at its transverselywidest portion, substantially full caliber in relation to barrel bore120-4. Also, certain embodiments of projectile 140 may be either wideror more slender relative the diameter of barrel bore 120-4 than theillustrated examples appear to be.

FIG. 1 depicts a side view of my invention in an embodiment whichcomprises blowgun 110 with associated subcaliber projectile 140 andassociated sabot means 170. FIG. 2 depicts a perspective view of blowgun110. Blowgun 110 includes elongate barrel 120 and, optionally,mouthpiece 130. Optional mouthpiece 130 is shown affixed to breech end120-3 of barrel 120. Barrel 120 is provided with breech opening 120-2,muzzle opening 120-6, and substantially straight, elongate bore 120-4which communicates between breech opening 120-2 and muzzle opening120-6. For convenience of illustration, FIG. 1 shows unobstructed sideviews of subcaliber projectile 140 and sabot means 170 prior to loadinginsertion and engagement within bore 120-4 of barrel 120; it should benoted, therefore, that in FIG. 1 the positioning and orientation ofsubcaliber projectile 140 and sabot means 170 relative each other andrelative blowgun 110 is simply for convenience of illustration andillustrates only one of many possible dispositions of subcaliberprojectile 140 and sabot means 170 prior to loading insertion andengagement within barrel bore 120-4. FIG. 2 depicts optional mouthpiece130 as frictionally engaged with breech end 120-3 of barrel 120. FIG. 2also shows an embodiment of optional mouthpiece 130 which is so adaptedas to engage the face of the user against the lips, or against the areaimmediately around the lips, or against both, advantageously sized andshaped with clearance to avoid any such contact with nose or chin aswould disrupt the positioning of optional mouthpiece 130 against face ofuser to achieve a good airseal, according to the manner of use depictedin FIGS. 17, 18, and 19.

Not illustrated: Alternatively, blowgun 110 may be operated withoutoptional mouthpiece 130, with no substantial loss in function, by theuser placing breech end 120-3 of barrel 120 directly against the face ina manner similar to that described above of engaging mouthpiece 130against face, or alternatively, may insert breech end 120-3 directlybetween lips and perhaps slightly inside mouth, and press lips firmlyaround and against outer surface 120-8 of barrel 120 to achieve a goodairseal. In a like manner, optional mouthpiece 130 may alternatively beso shaped and otherwise adapted as to engage the face of the user bybeing inserted between the user's lips and perhaps slightly inside theuser's mouth, with the user's lips pressed firmly around and againstouter surface of mouthpiece to achieve a good airseal. In suchembodiments that allow insertion of mouthpiece 130 or breech end 120-3between the lips and perhaps into the mouth, it is advantageous as asafety precaution to provide barrel 120 or mouthpiece 130 with anenlarged portion of sufficient width and suitable positioning to preventover-insertion of mouthpiece 130 or barrel 120 into the mouth or throatof the user.

Additional notes about optional mouthpiece 130: Optional mouthpiece 130,when used, may be so adapted or may be so provided with means as toenable mouthpiece 130 to be affixed or connected, either permanently orremoveably, to breech end 120-3 of barrel 120. Suitable means ofsecuring mouthpiece 130 to barrel 120 will be apparent to one skilled inthe art, and may include, for example, frictional engagement, orcooperating threaded sections that allow mouthpiece 130 and barrel 120to be screwed together. Such connecting means may involve direct contactbetween mouthpiece 130 and barrel 120, or alternatively may involvecontact through one or more intermediary members, such as, for example,a gasket or bushing, or a barrel extension member, or possibly ahardened matrix or filler layer such as molded plastic, cast metal, orglue or epoxy. Optional mouthpiece 130, or any intervening intermediarymember, may be essentially affixed to inner surface of bore 120-4, or toouter surface 120-8 of barrel 120, or to both. Means such as glue,epoxy, set screws, clamps, magnets with cooperating magneticallyattractive members, or detents, such as spring ball detents withcooperating indentations, may be used to appropriately strengthen ormake permanent various methods or configurations for affixing barrel 120and mouthpiece 130 together, such configurations even includingend-to-end abutting of barrel 120 and mouthpiece 130. Alternatively,methods of material working such as, for example, molding, casting,machining, and spinning may be used to form barrel 120 and mouthpiece130 as one unitary monolithic body rather than as two structurally ormaterially distinct elements.

FIG. 4 is a portion of the side view depicted in FIG. 1, enlarged toshow with greater clarity and detail a side view of subcaliberprojectile 140 and sabot means 170. Subcaliber projectile 140 in thisembodiment includes substantially straight, elongate, lightweighttubular shaft 160, affixed rearwardly to and advantageously coaxiallyaligned with relatively short, substantially straight, cylindricalforeshaft 150. FIG. 3 is a side view of foreshaft 150 by itself.Foreshaft 150 in this embodiment is advantageously provided with widerforward portion 150-2 and narrower rear portion 150-4. Sabot means 170in this embodiment includes advantageously thin-walled, advantageouslylightweight conical shell 170, sized and shaped at base 170-2 to besubstantially slidingly sealable with bore 120-4.

Note: It may be understood that in the embodiment depicted in FIGS.1-21, as well as in the embodiment depicted in FIGS. 22-43, foreshaftforward portion 150-2 is in fact somewhat wider than the outer diameterof shaft 160, but that certain illustrations within FIGS. 1-43 may showthe two components as apparently the same diameter, or with somewhatdifferent proportions or relative proportions, merely for convenience ofillustration. It will be apparent to one skilled in the art that variousembodiments of projectile 140 are possible in which the widest portionof foreshaft 150 is of diameter greater than, equal to, or less than theouter diameter of shaft 160.

Note: Subcaliber projectile 140 as depicted in FIG. 4 may be consideredas an exemplary embodiment of what may be considered a family ofstreamlined elongate subcaliber projectiles provided by my invention andwhich are particularly well suited for use with the blowgun provided bymy invention.

FIG. 4 continued: Sabot Cone 170 has base 170-2 sized and shaped tosubstantially match the caliber and cross-sectional shape (in thisembodiment, a circular disk shape) of barrel bore 120-4, firstly inorder that sabot 170 may form an adequate gas seal with bore 120-4 toprevent any significant leakage of pressurized air or breath past base170-2 during launch acceleration, and secondly in order that sabot base170-2 may frictionally engage the inner surface of bore 120-4 withsufficient snugness to resist or prevent axial displacement of sabot 170towards or out breech 120-2 when sabot 170 is loaded within bore 120-4of barrel 120 prior to launch acceleration, as set forth in theparticular manner of operation described below and depicted in FIGS.14-21. Thus cone 170 at its base 170-2 is substantially slidinglysealable with barrel bore 120-4, yet preferably without excessivefriction or snugness of fit, in order that breath (arrows 300, see FIGS.19-21) of the user may provide sufficient thrust to easily overcome thefrictional engagement between sabot means 170 and bore 120-4 to produceefficient launch acceleration

FIGS. 5 and 6 are, respectively, exploded and assembled perspectiveviews of subcaliber projectile 140. In this embodiment, subcaliberprojectile 140 includes foreshaft 150 and elongate shaft 160. Foreshaft150 is advantageously materially composed or structured or both in sucha manner as to have a high density or high linear density relative tothe density or linear density of shaft 160. Foreshaft 150 and shaft 160are further advantageously relatively proportioned and adapted in such amanner that subcaliber projectile 140 has a forward-of-center balance.In particular, the length of foreshaft 150 may preferably be somewhatshort relative the length of shaft 160 in order to help produce anoverall forward-of-center balance of subcaliber projectile 140, whiletaking into account any longitudinal overlap of portions of foreshaft150 and shaft 160. Shaft 160 is advantageously lightweight in order topromote the aforementioned forward-of-center balance and also in orderthat shaft 160 may thereby serve as an aerodynamic stabilizer forsubcaliber projectile 140. It will be apparent to one skilled in the artthat in embodiments in which there is little substantial overlap ofshaft 160 and foreshaft 150, and in certain other embodiments as well,foreshaft 150 need not be somewhat shorter than shaft 160, and couldeven be somewhat longer than shaft 160, while still achieving aforward-of-center balance or other balance determined appropriate, as iswithin the ability of those skilled in the art, in order that subcaliberprojectile 140 may have a stable balance and in order that, if sointended, shaft 160 may serve as an aerodynamic stabilizer forsubcaliber projectile 140.

Shaft 160, or foreshaft 150, or both, may alternatively be provided withadditional aerodynamic stabilizing means, as will be described in moredetail in the later section on alternate embodiments.

Continuing, FIG. 5 depicts an unobstructed perspective view of foreshaft150. Foreshaft 150 in this embodiment is provided with wider forwardportion 150-2 and narrower rear portion 150-4. Rear portion 150-4 isadvantageously proportioned and sized in such a manner as tofrictionally engage the inner surface of tubular shaft 160 when insertedinto forward opening 160-2 of shaft 160 in the manner depicted in FIG.6. The diameter of forward section 150-2 is advantageously somewhatgreater than the inner diameter of tubular shaft 160, and furthermore,the transition between forward section 150-2 and rear section 150-4 isadvantageously relatively abrupt, in order to provide a preferablyessentially perpendicular shoulder 150-3 against which forward end 160-3of shaft 160 may be securely abuttingly seated. An additional depictionof the manner of engagement between foreshaft 150 and shaft 160 isdepicted in sectional view in FIG. 11. Furthermore, in order to promoteaerodynamic stability of subcaliber projectile 140, the diameter of someportion of forward portion 150-2 is also advantageously wider than theouter diameter of forward end 160-3 of tubular shaft 160, in order toavoid any such reduction in the sectional density of the forward portionof subcaliber projectile 140 as might tend to destabilize projectile140.

Not illustrated: In some embodiments, in the event that outer diameterof rearward portion 150-4 of foreshaft 150 were to happen to besubstantially narrower than the inner diameter of shaft 160, foreshaft150 may be provided with intermediary means to maintain a secureconnection between foreshaft 150 and shaft 160. Such intermediary meansmight, for example, include one or more essentially sleeve-likeinsertion bushings or gaskets which slide onto and frictionally engagerearward section 150-4, and then which are inserted into andfrictionally engaged with the interior surface of forward end 160-3 ofshaft 160, thereby serving as one or more connecting intermediarymembers providing intermediary surface contact to maintain secureconnection between foreshaft 150 and shaft 160. A cushioning gasket orbushing may also be provided by either providing a widened forwardportion of the foremost insertion gasket or bushing, or alternatively bypositioning an additional, separate, wider gasket or bushing between theforeshaft shoulder 150-3 and the forward end of the insertion gasket orbushing. Such a cushioning intermediary body may help to reduce thepotential for any damage to forward end 160-3 of shaft 160 whensubcaliber projectile 140 impacts a target. Alternatively, if rearwardforeshaft section 150-4 is substantially narrower than the innerdiameter of shaft 160, a filler matrix such as epoxy may be used inplace of or in conjunction with insertion bushings or shoulder bushingsto fill any gaps in order to securely affix foreshaft 150 and shaft 160together and possibly to provide cushioning against impact shock. It ispreferable that the widest portion of any gasket or matrix left exposed,or in other words not covered or enclosed by some portion of shaft 160or foreshaft 150, which would likely be the cushioning portion, shouldbe of outer diameter not greater than the outer diameter of the widestportion of the forward portion 150-2 of foreshaft 150, in order topromote in-flight aerodynamic stability.

FIGS. 7-13: Point, or tip, 170-4 of sabot means 170 may be inserted intorearward opening 160-4 of shaft 160 of subcaliber projectile 140, sothat some portion of forward surface 170-6 of sabot 170 may therebyessentially rearwardly abuttingly engage subcaliber projectile 140. Inthis manner, subcaliber projectile 140 and sabot means 170 maycooperatively engage each other to form a functional unit which shall beknown as sabot projectile assembly 190 or sabot projectile 190, duringany or all of certain stages of the handling, loading, and launchingsequence; such stages possibly including, for example, while beinginserted into barrel bore 120-4 to assume loaded position, while beingmaintained in loaded position within bore 120-4 prior to launchacceleration, and while traveling along bore 120-4 during launchacceleration.

FIG. 7 and FIG. 8 depict, respectively, exploded and assembledperspective views of sabot projectile assembly 190. FIG. 9 and FIG. 10depict, respectively, side elevational and front elevational views ofsabot projectile assembly 190. The abutting engagement of subcaliberprojectile 140 rearwardly by sabot cone 170 provides a secure connectionwhereby sabot 170 may transmit positive thrust to subcaliber projectile140 during launch acceleration; at the same time, however, theessentially abutting engagement of subcaliber projectile 140 rearwardlyby sabot cone 170 preferably does not provide any substantial positiveconnection to prevent axial displacement of subcaliber projectile 140forwardly relative sabot means 170, nor to prevent axial displacement ofsabot cone 170 rearwardly relative subcaliber projectile 140. Theadditional loosely penetrative or nesting relationship in the engagementof sabot tip 170-4 inserted into subcaliber projectile shaft rearopening 160-4, prevents or resists premature lateral displacement ofsabot tip 170-4 relative shaft rear opening 160-4, and thereby furtherensures that subcaliber projectile 140 remains securely engagedrearwardly by sabot cone 170, while in loaded position within bore 120-4up until the commencement of launch acceleration, as well as duringlaunch acceleration and travel through and out bore 120-4. It should benoted that although FIGS. 7-13 appear to depict sabot 170 and subcaliberprojectile 140 as being substantially coaxially aligned when engagedtogether to form sabot projectile assembly 190, in actual operationentirely satisfactory results may be achieved even when sabot 170 isaxially aligned at somewhat of an angle to subcaliber projectile 140,and when either sabot 170 or subcaliber projectile 140 or both areaxially aligned at somewhat of an angle to barrel bore 120-4.

FIG. 11 depicts a sectional side view, along section line 11-11 fromFIG. 10, of sabot projectile assembly 190 in which shaft 160 is anelongate, essentially straight, hollow tubular member, preferably verylightweight. Foreshaft 150 advantageously includes wider forward section150-2 and narrower rear section 150-4. Rear section 150-4 is preferablyproportioned in such a manner as to frictionally engage the innersurface of shaft 160 when inserted into forward opening 160-2.Transition between forward section 150-2 and rear section 150-4advantageously is relatively abrupt, in order to provide essentiallyperpendicular shoulder 150-3 against which forward end 160-2 of shaft160 may be securely abuttingly seated.

Thus, some portion of forward portion 150-2 may advantageously besomewhat wider in diameter than rear section 150-4, so as to provideshoulder 150-3 against which forward end 160-3 of shaft 160 may besecurely abuttingly seated. Having some portion of forward portion 150-2be wider than shaft 160 not only may provide additional benefits interms of aerodynamic stability, as mentioned earlier, but may alsoprovide benefits in terms of target penetration performance with certaintypes of targets, since when penetrating such a target forward end 150-2clears or opens a penetration channel through which advantageouslynarrower shaft 160 may pass with little or no surface contact.

FIG. 12 depicts a sectional view, on a somewhat enlarged scale forclarity, of sabot projectile assembly 90 along section line 12-12 fromFIG. 9.

FIG. 12 shows foreshaft rear portion 150-4 inserted within, and therebyfrictionally engaged with, shaft 160, and outer diameter of shaft 160narrower than diameter of foreshaft shoulder 150-3.

FIG. 13 depicts a sectional view, on a somewhat enlarged scale forclarity, of sabot projectile assembly 190 along section line 13-13 fromFIG. 9.

FIG. 13 shows tip 170-2 of sabot cone 170 rearwardly inserted withinshaft 160 in order that sabot 170 may thereby abbutingly and looselypenetratively engage shaft 160.

FIG. 14 depicts a perspective view of a possible method by which theuser may manually hold subcaliber projectile 140 and sabot 170 engagedtogether as sabot projectile assembly 190, for manual handling of sabotprojectile assembly 190 preparatory to, and during, loading insertion ofsabot projectile assembly 190 into barrel breech 120-2 and therethroughinto barrel bore 120-4. It will be apparent to one skilled in the artthat there are other possible methods of manually holding sabotprojectile assembly 190 during loading and other handling. In the methoddepicted in FIG. 14, the user configures the fingers and thumb of onehand in approximately the position of preparing to snap the fingers.Subcaliber projectile 140 may, in this position of the hand, be grippedbetween thumb and middle finger, and sabot 170, with tip 170-2 insertedwithin rearward shaft opening 160-4, may be engaged rearwardly by theindex finger inserted rearwardly within the conical shell of sabot 170to push against rear surface 170-8 of sabot 170. In this manner, themutual opposition or constraint, of index finger against thumb andmiddle finger, is transmitted by sabot 170 and subcaliber projectile 140to each other, so that subcaliber projectile 140 and sabot 170 remainthereby securely engaged as sabot projectile assembly 190.

FIGS. 15 and 16 depict stages in a possible method of loading sabotprojectile assembly 190 into barrel bore 120-4 of blowgun 110. FIG. 15depicts the user holding blowgun 110 with barrel 120 uptilted so thatmuzzle 120-6 is higher than breech 120-2, and using the essentialtechnique, depicted above in FIG. 14, to hold subcaliber projectile 140and sabot 170 together, engaged as the functional unit known as sabotprojectile assembly 190. FIG. 15 further depicts sabot projectileassembly 190 as being partially inserted into breech 120-2 andtherethrough into and within bore 120-4, with the front end ofsubcaliber projectile 140 resting upon the inner surface of bore 120-4and the rearward portion of sabot projectile assembly 190 held andsupported by user's hand.

FIG. 16 depicts the user holding blowgun 110 in essentially the samemanner illustrated in FIG. 15, with sabot projectile assembly 190 fullyinserted into and within bore 120-4. In moving sabot projectile assembly190 from the first (partially loaded) position shown in FIG. 15, to thesecond (fully loaded) position shown in FIG. 16, as sabot projectileassembly 190 is pushed progressively further into and through breech120-2 by the pressure of the user's index finger upon sabot 170, theuser may gradually release the grip of thumb and middle finger uponsubcaliber projectile 140, allowing subcaliber projectile 140 to besupported in place with front end of foreshaft 150 slidingly supportedupon the inner surface of bore 120-4, and with rear end 160-5 of shaft160 supported upon sabot 170, with sabot 170 in turn supported on theindex finger. Accordingly, after releasing the grip of thumb and middlefinger upon sabot projectile assembly 190, the user may withdraw thumband middle finger out of the way to allow easier completion of loadinginsertion of sabot projectile assembly 190.

FIG. 17 depicts a partial perspective view of blowgun 110, with thedistal portion of barrel 120 cropped from view and with the portion atand near breech 120-2 and mouthpiece 130 partially cut away to showsabot projectile assembly 190 loaded within bore 120-4, with mouthpiece130 lifted to engage the mouth and lips of the user. FIG. 18 depicts aportion of FIG. 17 enlarged for greater clarity of detail.

FIGS. 17 and 18 depict sabot projectile assembly 190 in loaded positionwithin bore 120-4 after completion of loading insertion into and throughbreech 120-2 and before initiation of launch acceleration. Note thatbarrel 120, and particularly barrel bore 120-4, is uptilted with muzzle120-6 higher than breech 120-2 so that the urging of gravity maintainssubcaliber projectile 140 in seated position against or upon sabot 170.Sabot 170 is frictionally engaged by the inner surface of bore 120-4 andis thereby supported against urging of gravity, preferably firmly enoughto thereby secure sabot projectile assembly 190 against any excessiveaxial displacement towards or out breech 120-2 due to urging of gravity.In other words, sabot 170 is frictionally engaged by bore 120-4 withsufficient firmness that sabot 170 may support the weight of sabotprojectile assembly 190 when sabot projectile assembly 190 is loadedwithin bore 120-4 of barrel 120, uptilted with muzzle 120-6 higher thanbreech 120-2.

Note: with the foregoing in mind regarding the embodiment of myinvention depicted in FIGS. 1-21, it will be clear that during loading,and until launch is complete, barrel bore 120-4 should be maintained ator above the minimum angle of elevation sufficient to prevent prematureseparation of sabot means 170 and subcaliber projectile 140 due to theweight of subcaliber projectile 140 pulling subcaliber projectile 140away from secure engagement with sabot means 170. Thus, taking care topreserve a sufficient angle of elevation, the user may place breech end120-3 or mouthpiece 130, as appropriate, to engage his lips and mouthand blow therein to thereby initiate and produce launch acceleration ofsabot projectile assembly 190.

FIG. 19 shows sabot projectile assembly 190 partially displaced alongbore 120-4, traveling under launch acceleration through bore 120-4towards muzzle 120-6 (muzzle 120-6 is not shown in FIG. 19 due to imagecropping of the distal portion of barrel 120), propelled by thrust ofbreath (arrows 300) of user.

FIG. 20 depicts a perspective view of the distal portion of barrel 120,with the portion at and near muzzle 120-6 partially cut away to showsabot projectile assembly 190 partially exited through and out muzzle120-6. At this stage of launch, sabot projectile assembly 190 is stillmaintained as a functional unit by sabot 170 being positivelyaccelerated by thrust of breath (arrows 300) against the inertial massof subcaliber projectile 140. In this manner sabot projectile assembly190, in this embodiment of my invention, is maintained as a functionalunit until sabot 170 completely exits through and out muzzle 120-6, withaccompanying dispersal of thrust.

Not illustrated: In certain alternate embodiments or methods of use ofmy invention, subcaliber projectile 140 and sabot 170 may beginseparation before sabot 170 reaches or exits muzzle 120-6. An example ofsuch an alternate embodiment is one in which barrel 120 is ported, or inother words provided with air passage holes through wall of barrel 120and communicating between bore 120-4 and the exterior of barrel 120, toallow substantial dissipation of breath pressure and thrust prior tosabot 170 reaching or exiting muzzle 120-6. Such port holes wouldpreferably be placed in the distal portion of barrel 120 fairly nearmuzzle 120-6. An example of such an alternate method of use is when theuser uses a less forceful exhalation to launch sabot projectile assembly190, in such a manner that positive acceleration ceases before sabot 170exits muzzle 120-6.

FIG. 21 is a perspective view depicting discarding separation of sabot170 from subcaliber projectile 140 after sabot 170 has completed exitingthrough and out muzzle 120-6. After sabot 170 completes exiting throughand out barrel muzzle 120-6, and thereby breaks the substantial slidingairseal between sabot base 170-2 and the inner surface of barrel bore120-4, propulsive thrust (straight arrows 300) rapidly dissipates(curved arrows 310) and sabot 170 is no longer positively urged againstthe inertial mass of subcaliber projectile 140. Atmospheric drag(sharply bent arrows 320) acting upon sabot 170, which preferably has avery low sectional density compared to the sectional density ofsubcaliber projectile 140, causes sabot 170 to decelerate much morerapidly than subcaliber projectile 140, thus effecting separation anddiscarding of sabot 170 as subcaliber projectile 140 continues alone andunhindered along its external trajectory or path.

FIGS. 1-21 depict a preferred embodiment of my invention which comprisesa subcaliber projectile, sabot means, and blowgun, and in which thesubcaliber projectile includes a foreshaft and a shaft, and in which theblowgun includes an elongate barrel, and optionally, a mouthpiece. FIGS.22-43 depict a yet more preferred embodiment of my invention, which, inaddition to comprising essentially the same components as the embodimentdescribed in FIGS. 1-21, also further comprises a detent means to holdthe subcaliber projectile and sabot means together as a sabot projectileassembly and to hold said sabot projectile assembly in loaded positionwithin the bore, preferably until the commencement of launchacceleration. Briefly, in the embodiment depicted in FIGS. 22-43, thedetent means includes a projectile detent and a sabot detent whichcooperate in an essentially antagonistic manner to hold the sabotprojectile assembly in loaded position. In the embodiment depicted inFIGS. 22-43, the projectile detent includes a magnet, and the sabotdetent includes a means of partially obstructing the bore at or near thebreech, in order to thereby abbuttingly or frictionally engage the sabotrearwardly or laterally, after loading insertion, in order to preventthe sabot from moving therepast in the direction toward or out thebreech. Another change from the embodiment depicted in FIG. 1-21 is thatin the embodiment depicted in FIGS. 22-43, there is an additionalrequirement that some portion, or the entirety, of the foreshaft of thesubcaliber projectile (or some other suitable portion of the projectile)is composed of a material strongly susceptible to magnetic attraction,in order that the magnetic projectile detent may attract and hold thesubcaliber projectile when loaded within the bore, with the subcaliberprojectile engaged rearwardly by the sabot means, and the sabot means inturn engaged rearwardly by some portion of the sabot detent, until thecommencement of launch acceleration, when the thrust of the user'sbreath will cause the sabot and engaged subcaliber projectile to moveforward, the projectile foreshaft in a short distance breaking free ofthe magnetic projectile detent's influence, after which the sabot andsubcaliber projectile continue to accelerate together through and outthe bore of the barrel. Although certain embodiments, such as the onedepicted in FIGS. 22-43, which have a magnetic detent affixed externallyto the barrel, may function satisfactorily with a barrel composed inpart or in whole of steel or some other strongly magneticallyattractable material, in general such a barrel would tend to absorb someof the magnetic attraction and weaken the magnetic detent's influence onthe projectile. Therefore in certain embodiments with a magneticprojectile detent affixed externally to the barrel, such as the onedepicted in FIGS. 22-43, it will be advantageous if the barrel in itsentirety, or else in its portion against or close to the magneticdetent, is composed of some material such as aluminum, plastic, wood, orother suitable material which is essentially nonmagnetic andnon-susceptible to magnetic attraction.

Since the embodiment depicted in FIGS. 1-21 and the embodiment depictedin FIGS. 22-43 share many of the same components, many of the commentsin the above description, on methods of use and alternative versions ofembodiment, may be applied to the following description too, so I havenot repeated all of them, since it will be apparent to one skilled inthe art that they may apply to this embodiment as well. Since the maindifference between the two illustrated embodiments is the detent means,the applicant has focused on providing description and suggestions aboutpossible methods of use, and some of the possible alternatives, for thistype of detent. In terms of general all-around usage, the belowembodiment depicted in FIGS. 22-43 is more flexible than the aboveembodiment depicted in FIGS. 1-21, since the antagonistic detent meansmay be adapted, with the use of a sufficiently magnetically powerfulmagnetic detent, so as to constrain or confine the sabot projectileassembly in loaded position whether the barrel is up-tilted, horizontal,or downtilted, or in other words, in any desired orientation of thebarrel, and so that loaded positioning is secure even during fairlyvigorous handling of the blowgun. The secure positioning made possibleby the detent also means that the fit of the sabot within the bore maybe made slightly looser without causing premature sliding ordisplacement of the projectile assembly. The below embodiment depictedin FIGS. 22-43 may also develop higher launch velocities due to thepossibility of higher operating pressures, or earlier peaks in pressure,developing as a result of a slight travel delay imposed by the detentmeans, and also because the sabot may, if desired, be sized to fitslightly more loosely in the bore. Because of the many similarities,reading the below description of the blowgun depicted in FIGS. 22-43will probably also shed additional light on the function and means ofthe blowgun depicted in FIGS. 1-21.

FIG. 22 is a side view of my invention, in a preferred embodiment whichcomprises blowgun 110, associated subcaliber projectile 140, andassociated sabot means 170. Blowgun 110 in this embodiment includessubstantially straight elongate tubular barrel 120, detent means 200and, optionally, mouthpiece 130.

FIG. 23 depicts a perspective view of blowgun 110. Blowgun 110 includesadvantageously substantially straight elongate tubular barrel 120,detent means 200 and, optionally, mouthpiece 130. Barrel 120 is providedwith breech opening 120-2, muzzle opening 120-6, and substantiallystraight, elongate bore 120-4 which communicates between breech opening120-2 and muzzle opening 120-6. FIG. 23 depicts optional mouthpiece 130as frictionally engaged with breech end 120-3 of barrel 120. FIG. 23also shows optional mouthpiece 130 as being so adapted as to engage theface of the user against the lips, or against the area immediatelyaround the lips, or against both, with clearance to avoid any suchcontact with nose or chin as would disrupt the positioning of mouthpiece130 against face of user to achieve a good airseal, according to themanner of use depicted in FIGS. 38, 39, and 41.

FIG. 23 continued: In this embodiment, detent means 200 includesprojectile detent means 210 and sabot detent means 220. The significanceof the positioning of projectile detent 210 and sabot detent 220relative each other and relative barrel bore 120-4, will be explained inmore detail below. Sabot detent means 220 is preferably affixed to orintegral withd, or otherwise essentially contiguous with, the innersurface of barrel bore 120-4, at or near breech opening 120-2. Generallyspeaking, sabot detent means 220 may essentially comprise or include ashort section of bore of essentially reduced caliber, possibly providedby one or more bore indentations, or by one or more protrusions affixedto and protruding from the inner surface of bore 120-4, therebypartially obstructing bore 120-4. In this embodiment, sabot detent 220includes narrow ramp-like protrusion 220, affixed to and radiallyextending from the inner surface of bore 120-4 at or near breech 120-2,in such a manner that detent protrusion 220 is aligned lengthwisesubstantially parallel to the longitudinal axis of bore 120-4. Detentprotrusion 220 advantageously has a slanted surface facing rearwardstoward breech 120-2, and a shoulder surface facing forwards towardsmuzzle 120-6. During loading insertion of sabot 170, the rearward-facingsloped surface of detent 220 cooperates with the slanted forward sufaceof conical sabot 170 to more easily allow sabot 170 to be manuallypushed past sabot detent 220 in the direction towards muzzle 120-6during loading insertion. The forward-facing shoulder surface of detent220, upon contact with sabot means 170, abuttingly engages some portionof base 170-2 or other rearward-facing surface of sabot 170 in such amanner as to prevent or resist sabot cone 170, after completion ofloading insertion, from moving back past sabot detent 220 in thedirection towards or out of breech opening 120-2.

FIG. 23 continued: In this embodiment, projectile detent means 210includes magnet 210 externally affixed to or positioned against barrel120 at a predetermined distance, along barrel 120, from the position ofsabot detent means 220. The suitable positioning of magnetic detent 210relative sabot detent 220 may vary according to the particularembodiment, the particular method of use, and the particular userpreferences. In embodiments similar to the embodiment depicted in FIGS.22-43, the suitable distance, along barrel 120, between detent 210 anddetent 220 will typically correspond roughly to the length of assembledsabot projectile assembly 190, minus some portion of the length ofprojectile foreshaft 150, with the distance advantageously somewhat lessthan the total length of subcaliber projectile proper 140. Whenprojectile 140 is in loaded position, there may or may not be somelongitudinal or axial overlapping of the position of some magneticallyattractable portion of projectile 140 with the position of some portionof detent 210. The significance and suitability of the positioning ofthe projectile detent means 210 relative sabot detent means 220, andcertain advantageous characteristics desirable regarding the strengthand orientation of the magnetic field of detent 210, will become cleareras the description progresses, and will make it apparent to one skilledin the art that the suitability of positioning of projectile detent 210,relative bore 120-4 and relative sabot detent 220, may depend, amongother things, on the particular size, shape, polar orientation, andmagnetic field strength of magnetic detent 210, as well as on the size,shape and disposition, within projectile 140, of the portion ofprojectile 140 which is susceptible to magnetic attraction, as well ason the precise position, relative bore 120-4, at which some portion ofsabot detent 220 directly abbutingly engages sabot 170, as well as uponother factors such as the wall thickness of barrel 120, and the lengthfrom tip to base of sabot cone 170, as well as any longitudinal or axialoverlap (or alternatively gap between) of the position of somemagnetically attractable portion of projectile 140 with the position ofsome portion of detent 210 when projectile 140 is in loaded position.Furthermore, in certain embodiments, the predetermined relativepositioning (particularly the distance of separation along barrel 120),of detent 210 relative detent 220 may be selected from a certain rangeof functional relative positions, in order to allow tuning of variablessuch as initial launching resistance, in order to match user preference,comfort level, and ability.

FIG. 25 is a portion of the side view depicted in FIG. 22, enlarged toshow with greater clarity and detail a side view of subcaliberprojectile 140 and sabot means 170. Subcaliber projectile 140 in thisembodiment includes lightweight, substantially straight, elongatetubular shaft 160, which is preferably composed of resiliently flexibleplastic, affixed rearwardly to and coaxially aligned with substantiallystraight, relatively short, cylindrical foreshaft 150. FIG. 24 is a sideview of foreshaft 150 shown by itself. Foreshaft 150 in this embodimentis composed of, or includes a portion composed of, steel, iron, or othermaterial strongly susceptible to magnetic attraction. Shaft 160 andforeshaft 150 are advantageously relatively proportioned in such amanner that subcaliber projectile 140 has a forward-of-center balancesuch that hollow, lightweight shaft 160 may serve as an aerodynamicstabilizer, or in other words a means of applying aerodynamiccorrectional guidance to subcaliber projectile 140 during flight. Inthis embodiment, sabot means 170 includes lightweight conical shell 170sized and shaped at its base 170-2 to substantially, yet slightlyloosely, slidingly seal with barrel bore 120-4.

Sabot cone 170 is preferably composed or formed of a material such asmolded plastic, molded foam, plastic film, or paper, in order to therebyadvantageously be so adapted as to be very lightweight and waterresistant, and somewhat resiliently deformable or compressible at itsbase 170-2. Sabot cone 170 is further preferably so proportioned so thatthe angle formed in side profile by its point or vertex 170-4 isrelatively obtuse or blunt.

FIGS. 26 and 27 are, respectively, exploded and assembled perspectiveviews of subcaliber projectile 140. FIG. 26 includes an unobstructedperspective view of foreshaft 150. Foreshaft 150 in this embodiment isadvantageously provided with wider forward section 150-2 and narrowerrear portion 150-4. Rear portion 150-4 is advantageously proportionedand sized in such a manner as to frictionally engage the inner surfaceof tubular shaft 160 when inserted into the forward opening 160-2 ofshaft 160 in the manner depicted in FIG. 27. The diameter of forwardsection 150-2 is advantageously somewhat greater than the inner diameterof tubular shaft 160, and furthermore, the transition between forwardsection 150-2 and rear section 150-4 is advantageously relativelyabrupt, in order to provide preferably essentially perpendicularshoulder 153 against which forward end 160-3 of shaft 160 may besecurely abuttingly seated. An additional depiction of the manner ofengagement between foreshaft 150 and shaft 160 is depicted in sectionalview in FIG. 32. Furthermore, in order to promote aerodynamic stabilityof subcaliber projectile 140, the diameter of some portion of forwardportion 150-2 is also advantageously as wide as or wider than the outerdiameter of the forward end of tubular shaft 160, in order to avoidreducing the sectional density of the forward portion of subcaliberprojectile 140, and thereby helping to promote aerodynamic stability ofprojectile 140.

Point, or tip, 170-4 of sabot means 170 may be inserted into rearwardopening 160-4 of shaft 160 of subcaliber projectile 140, so that sabot170 may thereby essentially rearwardly abuttingly engage subcaliberprojectile 140 (FIGS. 28-34). In this manner, subcaliber projectile 140and sabot means 170 may cooperatively engage each other to form afunctional unit which shall be known as sabot projectile assembly 190 orsabot projectile 190, during any or all of certain stages of thehandling, loading, and launching sequence; such stages possiblyincluding, for example, while being inserted into barrel bore 120-4 toassume loaded position, while being maintained in loaded position withinbore 120-4 prior to launch acceleration, and while traveling along bore120-4 during launch acceleration.

FIG. 28 and FIG. 29 depict, respectively, exploded and assembledperspective views of sabot projectile assembly 190. FIG. 30 and FIG. 31depict, respectively, side elevational and front elevational views ofsabot projectile assembly 190. Sabot projectile assembly 190 includessubcaliber projectile 140 and sabot cone 170. Subcaliber projectile 140and sabot cone 170 are engaged as a functional unit in an essentiallyabutting manner by inserting forward tip 170-4 of sabot cone 170 intothe rear opening 160-4 of tubular shaft 160 of subcaliber projectile140. The tip angle of sabot cone 170 is preferably relatively blunt, asindicated above, in order to avoid any tendency to wedge into shaft 160and thereby either become jammed in shaft opening 160-4, or possiblysplit shaft 160. The rear portion of shaft 160 may, if necessary, bereinforced by methods such as a slight thickening of the shaft wall or awrapping of strong tape in order to provide enhanced protection againstany tendency of the tip of cone 170 to wedge into or split shaft 160.Before loading into barrel bore 120-4, subcaliber projectile 140 andsabot cone 170 have substantially no direct positive connection, and ifcone 170, after insertion into the rear of shaft 160, is not held theremanually or by some other external connecting means or external means ofsupport, then preferably cone 170 may freely drop out of and away fromshaft 160.

FIG. 32 depicts a sectional side view of sabot projectile assembly 190,along section line 32-32 from FIG. 31, in which shaft 160 is anelongate, essentially straight, hollow tubular member, preferably verylightweight. Foreshaft 150 advantageously includes wider forward section150-2 and narrower rear section 150-4. Rear section 150-4 is preferablyproportioned and sized in such a manner as to frictionally engage theinner surface of shaft 160 when inserted into forward opening 160-2. Thetransition between wider forward section 150-2 and narrower rear section150-4 advantageously provides essentially perpendicular shoulder 150-3against which forward end 160-2 of shaft 160 may be securely abuttinglyseated. Having some portion of forward portion 150-2 be wider than shaft160 not only may provide additional benefits in terms of aerodynamicstability, as mentioned earlier, but may also provide benefits in termsof target penetration performance, since when penetrating a target,forward portion 150-2 may clear or open a penetration channel throughwhich advantageously narrower shaft 160 may pass with little or nosurface contact.

FIG. 33 depicts a sectional view, on a somewhat enlarged scale forincreased clarity of detail, of sabot projectile assembly 190, alongsection line 33-33 from FIG. 30.

FIG. 33 shows tip 170-4 of sabot cone 170 rearwardly inserted withinshaft 160 in order that sabot 170 may thereby abbutingly and looselypenetratively engage shaft 160.

FIG. 34 depicts a sectional view, on a somewhat enlarged scale forincreased clarity of detail, of sabot projectile assembly 190 alongsection line 34-34 from FIG. 30.

FIG. 34 shows foreshaft rear portion 150-4 inserted within, and therebyfrictionally engaged with, shaft 160, with outer diameter of shaft 160narrower than outer diameter of foreshaft shoulder 150-3.

FIG. 35 depicts a perspective view of a possible method by which theuser may manually hold subcaliber projectile 140 and sabot 170 engagedtogether as sabot projectile assembly 190, for manual handling of sabotprojectile assembly 190 preparatory to, and during, loading insertion ofsabot projectile assembly 190 into barrel breech 120-2 and therethroughinto barrel bore 120-4. It will be apparent to one skilled in the artthat there are other possible methods of manually holding sabotprojectile assembly 190 during loading and other handling. In the methoddepicted in FIG. 35, the user configures the fingers and thumb of onehand in approximately the position of preparing to snap the fingers.Subcaliber projectile 140 may, in this position of the hand, be grippedbetween thumb and middle finger, and sabot 170, with tip 170-2 insertedwithin rearward shaft opening 160-4, may be engaged rearwardly by theindex finger inserted rearwardly within sabot conical shell 170 to pushagainst rear surface 170-8 of sabot 170. In this manner, the mutualopposition or constraint, of index finger against thumb and middlefinger, is transmitted by sabot 170 and subcaliber projectile 140 toeach other, so that subcaliber projectile 140 and sabot 170 remainthereby securely engaged as sabot projectile assembly 190.

FIG. 36 and FIG. 37 depict stages in a possible method of loading sabotprojectile assembly 190 into barrel bore 120-4 of blowgun 110. FIG. 36depicts the user holding blowgun 110 with one hand and with the otherhand using the essential technique, depicted above in FIG. 35, to holdsubcaliber projectile 140 and sabot 170 together, engaged as thefunctional unit known as sabot projectile assembly 190. FIG. 36 furtherdepicts sabot projectile assembly 190 as being partially inserted intobreech 120-2 and therethrough into and within bore 120-4, with the frontend or cooperating portion of subcaliber projectile 140 resting upon theinner surface of bore 120-4 and the rearward portion of sabot projectileassembly 190 held together and supported by the user's hand. FIG. 36depicts the user holding blowgun 110 oriented so that barrel bore 120-4is substantially horizontal; however it should be noted that in thisparticular embodiment, provided magnetic detent 210 is sufficientlystrong magnetically, the user could also load sabot projectile assembly190 while holding blowgun 110 with barrel bore 120-4 down-tilted so thatmuzzle 120-6 is lower than breech 120-2. Furthermore, sabot detent 220permits the user to load sabot projectile assembly 190 while holdingblowgun 110 with barrel bore 120-4 up-tilted so that muzzle 120-6 ishigher than breech 120-2, although barrel bore 120-4 will probably notnecessarily need to be uptilted during loading or when loaded, unlessprojectile detent 210 has somewhat low magnetic strength, or ispositioned or oriented in such a way as to exert a relatively weakinfluence on projectile 140.

FIG. 37 depicts the user holding blowgun 110 in essentially the samemanner illustrated in FIG. 36, with sabot projectile assembly 190 fullyinserted into and within bore 120-4. In moving sabot projectile assembly190 from the first (partially loaded) position shown in FIG. 36, to thesecond (fully loaded) position shown in FIG. 37, as sabot projectileassembly 190 is pushed progressively further into and through breech120-2 by the pressure of the user's index finger upon sabot 170, theuser may gradually release the grip of the thumb and middle finger uponsubcaliber projectile 140, allowing subcaliber projectile 140 to besupported in place with the front end of foreshaft 150 slidinglysupported upon the inner surface of bore 120-4, and with the rear end ofshaft 160 supported upon sabot 170, with sabot 170 in turn supported onthe user's index finger. Accordingly, after releasing the grip of thumband middle finger upon sabot projectile assembly 190, the user maywithdraw thumb and middle finger out of the way to allow easiercompletion of loading insertion of sabot projectile assembly 190. Uponcompletion of loading insertion, subsequent withdrawal of finger oroptional loading tool (loading tool not shown), sabot projectileassembly 190 will be held with sabot means 170 securely seated againstsabot detent 170, with the forward end of subcaliber projectile 140securely held against the inner surface of barrel bore 120-4, and withthe rearward end of subcaliber projectile 140 securely seated againstthe forward end or the forward surface of sabot cone 170, with a firmmutual opposition or close mutual confinement of subcaliber projectile140 against sabot means 170. It should be noted here that the insertionof sabot tip 170-4 within rear opening 160-4 of projectile shaft 160permits not only an essentially abutting engagement of subcaliberprojectile 140 rearwardly by some portion of sabot 170, but also permitswhat might be characterized as a loosely nesting or loosely penetrativeengagement of subcaliber projectile 140 by sabot cone 170, which servesto help prevent premature lateral displacement of projectile 140relative sabot cone 170. Additional notes about the relationship ofsabot projectile assembly components and detent components will followshortly below.

Note: Because of the substantial magnetic attraction possible betweendetent 210 and projectile 140 when they are sufficiently close together,when using the method of loading depicted in FIGS. 36 and 37, the usermay need to exercise some caution so that subcaliber projectile 140 isnot pulled forward by detent 210 away from secure engagement with sabot170 during loading insertion.

FIG. 37 continued: In this embodiment, detent means 200 includesprojectile detent means 210 and sabot detent means 220. Sabot detentmeans 220 is preferably affixed to or integral with the inner surface ofbarrel bore 120-4, at or near breech opening 120-2. Sabot detent means220 essentially comprises or includes a short section of bore ofessentially reduced caliber, possibly comprising one or more boreindentations, or one or more protrusions affixed to or integral with andprotruding from the inner surface of bore 120-4, thereby partiallyobstructing bore 120-4. In this embodiment, sabot detent 220 includesnarrow ramp-like protrusion 220, affixed to or integral with andradially extending from the inner surface of bore 120-4 at or nearbreech 120-2, in such a manner that detent protrusion 220 islongitudinally aligned substantially parallel to the longitudinal axisof bore 120-4. Detent protrusion 220 advantageously has a slantedsurface facing rearwards toward breech 120-2, and a shoulder surfacefacing forwards toward muzzle 120-6. The rearward-facing slanted surfaceof detent protrusion 220 cooperates with the slanted forward suface ofconical shell sabot 170 to more easily allow sabot 170 to be manuallypushed past sabot detent 220 in the direction towards muzzle 120-6during loading insertion. The forward-facing shoulder surface of detentprotrusion 220, upon contact with sabot means 170, abuttingly engagessome portion of base 170-2, or other rearward surface of sabot 170, insuch a manner as to prevent or resist sabot cone 170, after completionof loading insertion, from moving back past sabot detent 220 in thedirection towards or out of breech opening 120-2.

Note: FIGS. 22-43 appear to depict detent 210 and detent 220 withoutapparent connecting means to barrel/bore. However, each detent could beaffixed with glue/cemented in place with epoxy. One or both detents,particularly detent 220, could also be formed integrally with the wallstructure of barrel 120, or even affixed to or formed integrally withthe structure of optional mouthpiece 130, or even with an optionalbarrel extension member affixed intermediarily between barrel 120 andmouthpiece 130. It is also possible, if some proximal portion, orentirety, of barrel 120 is composed of steel or other stronglymagnetically attractable material, for detent 210 to be held in positionagainst barrel 120 by magnetic attraction, without need for any glue,epoxy, or other type of intermediary connecting means. However, such amagnetically attractable portion of barrel 120 would absorb some of themagnetic attraction of detent 210, thereby possibly weakening theinfluence of detent 210 upon projectile 140. Alternative connectingmeans will be apparent to one skilled in the arts and some possibilitiesare discussed further below.

Not illustrated: Although, with the embodiment depicted in FIGS. 22-43,users may employ the essentially simultaneous method depicted in FIGS.35-37 to load sabot projectile assembly 190 within bore 120-4, mostusers will probably find it as easy or easier to insert or load thecomponents of sabot projectile assembly 190 into bore 120-4 in asequential manner thusly: To begin, sabot projectile 140 is insertedinto breech opening 120-2 of bore 120-4 with foreshaft 150 forwardtowards muzzle 120-6 of barrel bore 120-4. The user inserts subcaliberprojectile 140 sufficiently far into bore 120-4 so that projectileforeshaft 150 (or other magnetically susceptible portion of projectile140) is held against the inner surface of bore 120-4 by the attractionof foreshaft 150 to magnetic projectile detent 210, in an initial,partially loaded position (Note: this method's initial, partially loadedposition is not illustrated and is likely different from the partiallyloaded position of the other method depicted in FIG. 36). Magneticprojectile detent 210 is advantageously positioned at a distance fromsabot detent 220 or breech 120-2 such that when subcaliber projectile140 is held against the inner surface of bore 120-4 in this initial,partially loaded position, a portion of the rearward end of shaft 160,preferably a short portion only, is still protruding out from breech120-2 of bore 120-4; or alternatively it is otherwise advantageous if,in this initial, partially loaded position, the rearward end of shaft 60is either flush with the rim of breech 120-2, or else withdrawn intobore 120-4 a distance away from breech 120-2 which is somewhat less thanthe axial length of sabot cone 170 measured from base 170-2 to tip170-4. The user may now release any manual hold on subcaliber projectile140 and leave projectile 140 held by magnetic detent 210 against theinside of bore 120-4, and preferably with rear end of shaft 160 near,at, or slightly protruding from breech 120-2 as described above. Theuser may now manually hold and handle sabot cone 170 with the freedhand, and thereby insert tip 170-4 of sabot cone 170 into rearwardopening 160-4 of subcaliber projectile shaft 160, and with subcaliberprojectile 140 thus engaged rearwardly in an essentially abutting mannerby sabot cone 170, push forward with index (or other) finger, or with anoptional insertion tool or mechanism (not shown), against the rearsurface of sabot cone 170, in the direction of muzzle 120-6, in order tocontinue inserting and loading sabot projectile assembly 190 into barrelbore 120-4. The user may continue pushing sabot cone 170 forward, withfinger or an optional insertion tool or mechanism (not shown), untilrearward base 170-4 of sabot cone 170 has been inserted into breech120-2 and has been pushed past the restriction of sabot detent 220 sothat sabot 170 may be rearwardly abuttingly engaged by sabot detent 220,at which time sabot projectile assembly 190 will be in a substantiallyfully-loaded position (Note: this fully-loaded position IS essentiallythe same as the fully loaded position shown in FIGS. 37, 38, 39 and 40).

FIGS. 37, 38 and 39 and 40: Whichever loading insertion method has beenused, when sabot projectile assembly 190 is at its fully-loadedposition, magnetic detent 210 and subcaliber projectile foreshaft 150(or other appropriate magnetically attractable portion of projectile140) should be relatively positioned such that the strength ofattraction between detent 210 and foreshaft 150 is still sufficient tohold the tip, or forward portion, or other cooperating portion ofsubcaliber projectile 140 against bore 120-4 securely enough that whenthe user completes loading insertion and stops pushing forward on sabot170 with finger or insertion tool, magnetic detent 210 may prevent orresist any further axial dislocation of sabot projectile assembly 190toward muzzle 120-6 prior to commencement of launch acceleration. Thus,in this embodiment it may be appreciated that projectile detent 210advantageously has a magnetic field of sufficient strength and size orrange to attract and hold subcaliber projectile 140 against the innersurface of bore 120-4, as projectile 140 moves along a range of motionor positionings corresponding in length of travel to somewhat more orless than the axial length from tip 170-4 to base 170-2 of sabot cone170, depending on the positioning of rearward end 160-4 of projectileshaft 160 relative breech 120-2 when subcaliber projectile 140 is ininitial partially loaded position, as described above.

Additional notes on advantageous positioning and orientation, and otherpreferable characteristics of the detent means, and on loading insertionof the sabot projectile assembly: When the user completes loadinginsertion and thereupon stops pushing sabot 170 forward in the directiontowards muzzle 120-6 with finger or optional insertion tool, andsubsequently withdraws the finger or insertion tool back out of breech120-2, sabot 170 may in some embodiments or situations be able to movebackwards toward breech 120-2 a short distance before contacting andsecurely abbuttingly engaging some portion of sabot detent 220.Accordingly, in such embodiments magnetic detent 210 is advantageouslypositioned, oriented and of sufficient magnetic strength that whenloading insertion is completed, some component of the attractive forcebetween projectile foreshaft 150 and magnetic detent 210 willresiliently urge subcaliber projectile 140 towards breech 120-2.Typically, such a magnetically imposed breechward urging may beaccomplished in part by positioning some portion of detent 210 somewhatlongitudinally behind (that is, closer to detent 220 than) thelongitudinal center of the magnetically attractable portion ofprojectile 140, or in other words positioning detent 210 so that thedistance between detent 210 and detent 220 is less than the distancebetween detent 220 and the longitudinal center (or otherwise locatedcenter-of-mass or center of magnetic response) of the magneticallyattractable portion of projectile 140. Or in other words, such amagnetically imposed breechward urging may be accomplished in part bypositioning some portion of detent 210 between the center-of-mass orcenter of magnetic response of the magnetically attractable portion ofprojectile 140, and detent 220. Advantageously, such a magneticallyimposed breechward urging should tend to cause subcaliber projectile 140to slide backward upon and within bore 120-4 in immediate followingresponse to any backward or breechward motion of sabot cone 170, so thatthe withdrawing of the user's finger or optional insertion tool is ineffect executed under a magnetically produced backpressure transmittedby subcaliber projectile 140 to sabot cone 170 that keeps sabot cone 170followingly pressed against the withdrawing finger tip or insertion tooluntil some rearward portion of sabot cone 170 is securely abuttinglyengaged by sabot detent 220. Such a backpressure may make possible avery smooth and sensitive following motion by sabot projectile assembly190 of the withdrawing finger or insertion tool so that at no timeduring the withdrawal is there any significant break in continuouscontact between sabot cone 170 and the rear end of projectile 140, noris there any significant break in contact between the rear surface ofsabot cone 170 and the withdrawing finger or insertion tool, until suchtime as sabot detent 220 abuttingly engages the rear of sabot cone 170and thereby constrains cone 170 from further axial displacement in thedirection towards or out breech 120-2. Such substantially continuous,unbroken contact helps to prevent or resist any excessive axial orlateral dislocation of sabot cone 170 relative subcaliber projectile 140during loading insertion and positioning. It should be noted that ifmagnetic detent 210 has a magnetic field sufficiently strong, detent 210may advantageously be oriented with its axis or direction of strongestmagnetic pull obliquely tilted relative the longitudinal axis of barrelbore 120-4, rather than aligned parallel to or perpendicular to thelongitudinal axis of barrel bore 120-4 (such an obliquely tiltedorientation of detent 210 is not shown in the illustration figures).Such an obliquely tilted alignment of detent 210 may have an effect ofstrengthening the breechward component of the magnetic urging uponprojectile foreshaft 150, while at the same time may somewhat diminishthe component of magnetic attraction that attempts to pull foreshaft 150down against the inner surface of bore 120-4 (such as the component ofmagnetic attractive force that is essentially normal to the innersurface of bore 120-4). If the magnetic field pulls subcaliberprojectile 140 too firmly against the inner surface of bore 120-4, theresulting frictional engagement may become too strong to allowsubcaliber projectile 140 to backslide smoothly towards breech 120-2under the urging of the breechward component of the magnetic influenceof detent 210, in following response to any breechward motion of sabotmeans 170. It is within the ability of those skilled in the art todetermine suitable positioning, orientation, and magnetic fieldcharacteristics of one or more magnets relative bore 120-4 and relativesabot detent 220 in order that the magnet or magnets may tend to causethe aforementioned advantageous breechward urging of the appropriate,cooperatingly positioned and oriented magnetically attractable portionof projectile 140, while advantageously not tending to cause theaforementioned excessively firm or strong pulling of projectile 140against the inner surface of bore 120-4, in order to thereby promote theaforementioned substantially smooth following motion by sabot projectile190 of the withdrawn finger or optional insertion tool after loadinginsertion, in order to tend to cause the aforementioned substantiallycontinuous, unbroken contact between components of sabot projectile 190that would tend to prevent or resist any excessive axial or lateraldislocation of sabot cone 170 relative subcaliber projectile 140, andany optional intermediary members, during loading insertion andpositioning of sabot projectile 190.

FIG. 39 is a portion of the side view depicted in FIG. 38, enlarged toshow with greater clarity and detail a side view of sabot projectileassembly 190 confined in fully loaded position by the mutual oppositionor mutual confinement imposed by projectile detent means 210 and sabotdetent means 220. The somewhat enlarged side view depicted in FIG. 39also clearly shows a slight flexing of resiliently flexible shaft 160which may possibly occur when sabot projectile assembly 190 is confinedin loaded position within bore 120-4 by detent means 200, and with thesubstantial length of foreshaft 150, along with any overlapping portionof shaft 160, pulled substantially against or parallel to the innersurface of bore 120-4 by the attractive pull between projectile detent210 and foreshaft 150. It will be apparent to one skilled in the artthat alternate embodiments are possible in which shaft 160 or projectile140 is relatively rigid and in which, for example, only the forward tipof foreshaft 150 or projectile 140 would be pulled against the innersurface of bore 120-4 by detent 210. It will also be apparent to oneskilled in the art that in certain embodiments, due to, for example,sufficient flexibility of the structure of sabot 170, or sufficientlooseness of fit of sabot 170 within bore 120-4, there may be sufficientplay in the orientation of sabot 170 within bore 120-4 that sabot 170may tilt at a sufficient angle relative the longitudinal axis of bore120-4 so that sabot 170 may thereby engage with its tip, or otherappropriate cooperating portion, some portion of projectile 140 that issubstantially against the inner surface of bore 120-4. Sabot detentmeans 220 is preferably affixed to or integral with the inner surface ofbarrel bore 120-4, at or near breech opening 120-2. In this embodiment,sabot detent 220 includes narrow ramp-like protrusion 220, affixed toand radially extending from the inner surface of bore 120-4 at or nearbreech 120-2, in such a manner that detent protrusion 220 is alignedlengthwise substantially parallel to the longitudinal axis of bore120-4. Sabot detent protrusion 220 advantageously has a slanted surfacefacing rearward toward breech 120-2, and a shoulder surface facingforward toward muzzle 120-6. The rearward-facing slanted surface ofdetent protrusion 220 may cooperate with the slanted forward suface ofsabot 170 to more easily allow sabot 170 to be be manually pushed pastsabot detent 220 in the direction towards muzzle 120-6 during loadinginsertion. The forward-facing shoulder surface of detent protrusion 220,upon contact with sabot means 170, abuttingly engages some portion ofbase 170-2 or other rearward surface of sabot 170 in such a manner as toprevent or resist sabot cone 170, after completion of loading insertion,from moving back past sabot detent 220 in the direction towards or outof breech opening 120-2.

FIG. 40 is a sectional view along section line 40-40 from FIG. 39,showing sabot 170 rearwardly engaged by sabot detent means 220, and withprojectile detent 210 and optional mouthpiece 130 each externallyaffixed to barrel 120. It may be noted that in general, sabot detentmeans 220 partially obstructs bore 120-4 in such a manner as to preventor resist sabot cone 170, after completion of loading insertion, frommoving past, or back past, sabot detent 220 in the direction towards orout of breech opening 120-2, and particularly to prevent sabot 170 frombeing sucked out through breech 120-2 by the user, and as well toprevent sabot 170 from either falling out through breech 120-2 due togravity or reorientation of bore 120-4, or being pushed out throughbreech 120-2 due to any backpressure, such as any backpressure possiblyimposed by magnetic detent 210 and trans-mitted by subcaliber projectile140 to sabot 170, as was described above, or such as any backpressurepossibly imposed by any spring bias due to any flexing of anyresiliently flexible portion of projectile 140 or sabot 170 or otherpossible projectile assembly component.

FIG. 40 helps to make it evident that, furthermore, in this embodiment,sabot detent means 220 may partially obstruct bore 120-4 in such amanner as to preferably cause little or no substantial reduction inairflow through bore 120-4, and also so as to preferably allowrelatively easy manual insertion, with finger or possibly with the aidof an optional insertion tool, of preferably somewhat pliable,deformable, or compressible sabot cone 170 past sabot detent 220 in thedirection towards muzzle 120-6. Sabot detent means 220 is preferablyaffixed to or integral with the inner surface of barrel bore 120-4, ator near breech opening 120-2. Sabot detent means 220, in broader termsthat may apply to this embodiment or to certain alternative embodiments,essentially comprises or includes a short section of bore of essentiallyreduced caliber, which may be provided, for example, by one or more boreindentations, or by one or more protrusions essentially affixed to orintegral with and protruding from the inner surface of bore 120-4,thereby partially obstructing bore 120-4. It will be apparent to oneskilled in the art that sabot detent extension 220 might be wider, yetshorter, or less radially protrusive, than shown in FIG. 40, in order tostill avoid excessively obstructing airflow, and that additionally, oralternatively, some portion of sabot detent extension 220 might beshaped to essentially define one or more portions of an essentiallyannular shoulder or rim essentially contiguous with the inner surface ofbore 120-4.

FIGS. 37, 38, 39, and 40, continued: Upon completion of loadinginsertion, withdrawal of finger or optional loading tool or mechanism,and any corresponding breechward following motion by sabot projectileassembly 190, sabot projectile assembly 190 will be held in fully loadedposition, with sabot means 170 securely seated against sabot detent 170,with the forward end of subcaliber projectile 140 securely held againstthe inner surface of barrel bore 120-4, and with the rearward end ofsubcaliber projectile 140 securely seated against forward end or surfaceof sabot cone 170, preferably with a firm mutual opposition or closemutual confinement of subcaliber projectile 140 against sabot means 170.It should be noted here that the insertion of sabot tip 170-4 withinrear opening 160-4 of projectile shaft 160 permits not only anessentially abutting engagement of subcaliber projectile 140 rearwardlyby some portion of sabot 170, but also permits what might becharacterized as a loosely nesting or loosely penetrative engagement ofsubcaliber projectile 140 by sabot cone 170, which serves to helpprevent premature lateral displacement of subcaliber projectile 140relative sabot cone 170. Any such premature lateral displacement, ifexcessive, could result in dislocation of sabot cone tip 170-4 fromwithin the effectual socket of rear opening 160-4 of projectile shaft160, which loss of secure engagement would likely cause sabot cone 170to fail to efficiently transmit thrust to subcaliber projectile 140during launch acceleration, likely causing a jam within bore 120-4, ofprojectile 140 squeezed side by side against sabot 170, or else possiblycausing preferably somewhat deformable or compressible sabot cone 170 toslide over and past preferably slender subcaliber projectile 140,thereby causing sabot 170 to accelerate alone and without projectile 140through bore 120-4 and out from muzzle 120-6.

Note: Optional loading tool or mechanism for inserting sabot projectileassembly 190 into bore 120-4 is not shown in the illustration figures.In some embodiments, it might not be necessary to withdraw or removesuch a loading tool or mechanism before initiating launch, particularlyif such a tool or mechanism is part of a mechanical action used to loador “chamber” sabot projectile assembly 190.

Note: Although most users will probably find it easier and moreconvenient for projectile detent 210 to be affixed to barrel 120 eitherdirectly or via one or more intermediary connecting members, it shouldalso be noted that in some embodiments magnetic detent 210 need not beaffixed at all to barrel 120, but could instead, for example, even beheld manually in place against or sufficiently near barrel 120 by one ofthe user's hands, or by some other external means of supporting detent210 in place against or sufficiently near barrel 120. It should also benoted that any flexing of preferably resiliently flexible shaft 160, orof any other resiliently flexible portion of sabot projectile assembly190, when sabot projectile assembly 190 is confined in fully loadedposition, may contribute a spring bias tension that helps to keep therear end of subcaliber projectile 140 pressed securely against theforward end or forward surface of sabot 170, and possibly also helpingto keep rearward surface of sabot 170 pressed securely against sabotdetent 220.

FIGS. 37, 38, 39, and 40, continued: Sabot projectile assembly 190 isnow held securely in fully loaded position, not only by the pulling ofthe forward portion or tip of subcaliber projectile 140 against theinner surface of bore 120-4 by the magnetic attraction of projectiledetent 210, along with the attendant frictional engagement of subcaliberprojectile 140 by the inner surface of bore 120-4, but also by themutual opposition of the breechward urging of magnetic detent 210 uponsubcaliber projectile 140, countered by the abutting engagement of sabotcone 170 against sabot detent 220. As long as magnetic detent 210 issufficiently strong magnetically, and positioned and orientedappropriately relative foreshaft 150, then sabot projectile assembly 190will be held very substantially securely and somewhat resiliently inloaded position, so that blowgun 110 may be handled and reoriented withlittle fear of displacing sabot projectile assembly 190 from its loadedposition within bore 120-4, unless blowgun 110 is subjected to a rathersevere jolt or shock or perhaps dropped or swung violently. In addition,the positioning effect imposed upon sabot projectile assembly 190 withinbore 120-4, caused by the mutual opposition of magnetic detent 210 andsabot detent 220, as well as by the pulling of foreshaft 150 against theinner surface of bore 120-4 by the attraction of magnetic detent 210,may result in a very consistent, repeatable shot-to-shot positioning andorientation of sabot projectile assembly 190, and in particular of sabotprojectile proper 140, which consistency effect may substantiallyenhance accuracy performance. Based on the preceding explanation, itwill be apparent to one skilled in the art how to position and orientdetent 210 and detent 220, and how to select other characteristics ofdetent 210, detent 220, and projectile 140 to achieve secure loadedpositioning and other loading insertion and positioning actions andcharacteristics described or suggested above.

FIG. 41 shows sabot projectile assembly 190 partially displaced alongbore 120-4, traveling under launch acceleration through bore 120-4towards muzzle 120-6 (muzzle 120-6 is not shown in FIG. 41 due to imagecropping of the distal portion of barrel 120), propelled by thrust ofbreath (arrows 300) of user.

FIG. 42 depicts a perspective view of a distal portion of barrel 120,with the portion at and near muzzle 120-6 partially cut away to showsabot projectile assembly 190 partially exited through and out muzzle120-6. At this stage of launch, sabot projectile assembly 190 ispreferably still maintained as a functional unit by sabot 170 beingpositively accelerated by thrust of breath (arrows 300) against theinertial mass of subcaliber projectile 140. In this manner sabotprojectile assembly 190, in this embodiment of my invention, ispreferably maintained as a functional unit until sabot 170 completelyexits through and out muzzle 120-6, with accompanying dispersal ofthrust.

Not illustrated: In certain other alternative embodiments or methods ofuse of my invention, subcaliber projectile 140 and sabot 170 may beginseparation before sabot 170 reaches or exits muzzle 120-6. An example ofsuch an alternate embodiment is one in which barrel 120 is ported, or inother words provided with air passage holes through the wall of barrel120 and communicating between bore 120-4 and the exterior of barrel 120,to allow substantial dissipation of breath pressure and thrust prior tosabot 170 reaching or exiting muzzle 120-6. Any such port holes wouldpreferably be placed in the distal portion of barrel 120 fairly nearmuzzle 120-6. Another example of such an alternate embodiment is one inwhich barrel bore 120-4 is substantially flared near muzzle 120-6, or inwhich bore 120-4 is of sufficient length that air pressure of thrustdeclines to the point that sabot projectile assembly 190 is notpositively urged through bore 120-4 all the way to muzzle 120-6.Similarly, in an example of such an alternate method of use, the usermay blow relatively softly so that sabot 170 is not positively urgedthrough bore 120-4 all the way to muzzle 120-6.

FIG. 43 is a perspective view depicting discarding separation of sabot170 from subcaliber projectile 140 after sabot 170 has completed exitingthrough and out muzzle 120-6. After sabot 170 completes exiting throughand out barrel muzzle 120-6, and thereby breaks the substantial slidingairseal between sabot base 170-2 and the inner surface of barrel bore120-4, propulsive thrust (straight arrows 300) rapidly dissipates(curved arrows 310) and sabot 170 is no longer positively urged againstthe inertial mass of subcaliber projectile 140. Atmospheric drag(sharply bent arrows 320) acting upon sabot 170, which preferably has avery low sectional density compared to the sectional density ofsubcaliber projectile 140, causes sabot 170 to decelerate much morerapidly than subcaliber projectile 140, thus effecting separation anddiscarding of sabot 170 as subcaliber projectile 140 continues alone andunhindered along its external trajectory or path.

FIGS. 41, 42, and 43, continued: After loading is completed, the usermay launch projectile 140 when desired by placing either breech 120-2 oroptional mouthpiece 130 to his mouth and lips and blowing therein. Thepressure of the user's breath received into breech 120-2 of bore 120-4,either directly or via optional mouthpiece 130, establishes a pressuredifferential across the effectual piston of sabot means 170. As pressurebuilds and the pressure differential becomes sufficient to overcome theinitial launching resistance, sabot projectile assembly 190 begins tomove forward, breaking free in a short distance of the influence ofmagnetic detent 210 and traveling forward under positive acceleration,secured by inertia as a functional unit, through and from bore 120-4 ofbarrel 120. After exiting barrel muzzle 120-6, air pressure and thrustrapidly disperse and sabot cone 170 is consequently no longer positivelyurged against the inertial mass of subcaliber projectile 140;furthermore, since subcaliber projectile assembly 190 was removed fromthe mutual opposition of antagonistic detent means 200 in the earlystages of launch acceleration, sabot projectile assembly 190 maycommence travel along its external trajectory with negligible orvirtually no positive connection of sabot cone 170 to subcaliberprojectile 140, since the essentially abutting engagement of sabot cone170 to subcaliber projectile 140 preferably does not provide anysubstantial positive connection to prevent axial displacement ofsubcaliber projectile 140 forwardly relative sabot means 170, nor ofsabot cone 170 rearwardly relative subcaliber projectile 140. Indeed, aswas mentioned above, prior to loading, subcaliber projectile 140 andsabot cone 170 may naturally tend to disengage and fall apart if notexternally supported or constrained against each other, even when theyhave essentially no forward velocity at all. Upon exiting muzzle 120-6at the completion of launch acceleration, on the other hand, subcaliberprojectile 140 and sabot 170 may each have a very substantial forwardvelocity. Furthermore, since subcaliber projectile 140 is advantageouslyof an elongate, slender shape with a relatively small frontal profile,sabot means 170 (which is following behind with a preferably relativelymuch larger frontal profile) will advantageously have a substantialportion of its lateral area immediately exposed to and directly actedupon by atmospheric drag. Relative to subcaliber projectile 140, sabotcone 170 advantageously has a comparatively very light mass and very lowsectional density, with the result that atmospheric drag will causesabot means 170 to decelerate much more rapidly than subcaliberprojectile proper 140, thereby actuating separation of sabot cone 170from subcaliber projectile 140 so that discarding of sabot cone 170occurs and subcaliber projectile 140 continues alone and unhindered totravel along its external trajectory. Thus it may be appreciated thatthe substantial lack of positive connection, as described above, ofsabot cone 170 to subcaliber projectile 140, once they are removed fromthe influence of any external connecting means and sabot cone 170 is nolonger positively urged by launching thrust against the inertial mass ofsubcaliber projectile 140, results in a very quick, clean separation anddiscarding of sabot 170, with substantially little or no transmission ofdrag, impulse, torque, or other perturbations from sabot means 170 tosubcaliber projectile 140 during the discarding process.

Not illustrated: Some notes on a do-it-yourself version/embodimentsimilar to the embodiment depicted in FIGS. 22-43 will be includedfurther below in the section on alternate embodiments.

FIGS. 44-46 depict another embodiment of my blowgun chosen for detaileddescription to help illustrate the wide range of applications to whichmy invention is suited, and also because this embodiment is also wellsuited for adaptation as a do-it-yourself kit, as will be described inmore detail in the section on alternative embodiments. The embodimentdepicted in FIGS. 44-46 comprises blowgun 110 with associated subcaliberprojectile 140 and associated sabot means 170.

FIG. 44 is a side elevation view of blowgun 110 with subcaliberprojectile 140 and sabot means 170 in loaded position within blowgun110.

FIG. 45 is a perspective view of subcaliber projectile 140 and sabotmeans 170, both of which are advantageously adapted to cooperatinglyabbutingly engage each other to form sabot projectile assembly 190during any or all of certain stages in the handling, loading, andlaunching sequence. FIG. 45 shows projectile 140 and sabot 170 as theymay appear during the early stages of sabot discarding shortly afterexit from muzzle 120-6 at the completion of launch acceleration.

FIG. 46 shows an exploded perspective view of blowgun 110, withprojectile 140 and sabot 170 depicted as they may essentially appear inthe initial orientation of travel along their respective externaltrajectories or paths, shortly after exit from muzzle 120-6 at thecompletion of launch acceleration.

FIGS. 44-46, continued. Blowgun 110 includes substantially elongatebarrel 120, detent means 200, and, optionally, mouthpiece 130. Optionalmouthpiece 130 is shown affixed to breech end 120-3 of barrel 120.Barrel 120 is provided with breech opening 120-2, muzzle opening 120-6,and substantially straight, elongate bore 120-4 which communicatesbetween breech opening 120-2 and muzzle opening 120-6. Sabot means 170in this embodiment comprises essentially solid cylindrical sabot 170.Cylindrical sabot 170 is preferably composed of resiliently compressibleopen cell foam, advantageously composed of plastic or rubber.Cylindrical sabot 170 preferably is transversely sized and shaped to beloosely slidably sealable with bore 120-4. Cylindrical sabot 170preferably has some longitudinal dimension, or longitudinal axiallength, somewhat greater than the caliber of bore 120-4, in order totend to prevent sabot 170 from tumbling sideways or endover-end duringtravel down the bore during launch. Subcaliber projectile 140 in thisembodiment comprises a steel BB shot of the general type commonly usedin 177 caliber or other caliber mechanical airguns. Accordingly, thecaliber of barrel bore 120-4 in this embodiment may be considered topreferably fall into a smallbore range of calibers, preferably generallyin the range from 25 caliber to 35 caliber. Somewhat smaller or largercalibers may be used. Barrel 120 may advantageously be supplied in thisembodiment by a portion of a stock tubular arrow shaft of the kind usedin archery and commonly made of aluminum or carbon fiber. Detent means200 comprises a magnetic projectile detent 210 and sabot detent 220.Projectile detent 210 in this embodiment comprises doughnut-shaped orring-shaped magnet 210 affixed externally to barrel 120 or to optionalmouthpiece 130, preferably near breech 120-2. Sabot detent 220, in thisparticular muzzle-loading embodiment of blowgun 110, comprises narrowcrossbar 220 affixed essentially within and extending transverselywithin and across bore 120-4, preferably near breech 120-2. Barrel 120is provided with two small holes near breech 120-2, with holescooperatingly sized and shaped for snug insertion therethrough andaffixing therein of detent crossbar 220; additional or alternative meansof affixing or securing crossbar 220 in place will be apparent to oneskilled in the art. Magnetic detent 210 advantageously generates asufficiently strong magnetic attraction upon projectile 140 to therebyhold projectile 140 in place in loaded position either against the innersurface of barrel bore 120-4, or against the forward end of sabot means170, or both.

It will be apparent to one skilled in the art that in certainembodiments magnetic detent 210 need not necessarily comprise aring-shaped or donut-shaped magnet, and that projectile detent 210 incertain embodiments need not be positioned along barrel 120 betweensabot detent 220 and breech 120-2. It will be apparent to one skilled inthe art that projectile detent 210, or sabot detent 220, or both, mayalternatively be affixed to or affixed within cooperating portions ofmouthpiece 130, and in certain such embodiments, when mouthpiece 130 isaffixed to barrel 120, magnetic detent 210, or sabot detent 220, orboth, would be positioned beyond, or behind, breech 120-2, or in otherwords, magnetic detent 210, or sabot detent 220, or both, would bepositioned so as to not longitudinally overlap barrel 120 in respect tothe longitudinal axis of barrel 120. Accordingly, depending on thespecific embodiment, sabot detent 220 or projectile detent 210 or bothmay be affixed to, or integral with, either barrel 120, or additionallyor alternatively mouthpiece 130, if optional mouthpiece 130 is used inthe particular embodiment. If both sabot detent 220 and projectiledetent 210 are affixed to or integral with mouthpiece 130, thenprojectile detent 210 may in some such embodiments be positioned closerto the air inlet end of mouthpiece 130 than is sabot detent 220. Thuscertain suggested embodiments, of the BB-launching sabot projectileblowgun under consideration, exemplify some of the possible alternaterelative positioning of elements of detent 200 such as projectile detent210 and sabot detent 220.

FIGS. 44-46, continued. To load sabot 170 and projectile 140 intoblowgun 110, the user may according to one possible method of use holdbarrel 120 with bore 120-4 tilted muzzle upward, preferably with barrelbore 120-4 substantially vertical. The user may then sequentially loadthe components of sabot projectile assembly 190 by inserting foamcylinder sabot 170 into and through muzzle 120-6, and then inserting BBshot 140 into and through muzzle 120-6. The fit of sabot 170 within bore120-4 is preferably loose enough that the weight of BB projectile 140pressing downwards on top of sabot 170 is sufficient to make the sabot170, along with the other components of sabot projectile assembly 190,slide down bore 120-4 until the rear end of sabot 170 engages crossbardetent 220. If necessary, optional means, such as a ramrod, or a weighton a string, or other suitable means, can be used to push against or addweight on top of sabot 170 or sabot projectile assembly 190 and therebyforce sabot 170 or sabot projectile assembly 190 to slide down bore120-4 to engage crossbar 220. When sabot 170 engages crossbar 220, andprojectile 140 forwardly engages sabot 170, so that sabot projectileassembly 190 assumes a loaded position, projectile 140 should be closeenough to magnetic projectile detent 210 that steel BB shot 140 iswithin the influence of the magnetic attraction exerted by projectiledetent 210. The attraction between magnetic detent 210 and BB shot 140may thereby keep BB shot 140 pressed firmly against sabot 170, withsabot 170 in turn kept firmly pressed against sabot detent crossbar 220,even when barrel bore 120-4 is reoriented away from the vertical, orotherwise uptilted, position advantageously assumed during loading. BBshot 140 may or may not be in contact with the inner surface of bore120-4 when held in this manner against the sabot 170.

FIGS. 47-51 depict an embodiment of my blowgun which comprises blowgun110 and optional full caliber projectile 600. Blowgun 110 comprisessubstantially elongate barrel 120 and optional mouthpiece 130. Barrel120 is provided with breech opening 120-2, muzzle opening 120-6, andsubstantially straight, elongate bore 120-4 which communicates betweenbreech opening 120-2 and muzzle opening 120-6. Bore 120-4 is providedwith guidance means 500 disposed in or on the inner surface of bore120-4.

FIG. 47 is a perspective view of blowgun 110, partially cut away at andnear breech 120-2 and mouthpiece 130 to show optional projectile 600 inloaded position within bore 120-4 near breech 120-2. The inner surfaceof bore 120-4 is provided with guidance means 500. In this embodiment,guidance means 500 comprises elongate, essentially straight groove 500.Groove 500 is advantageously cross-sectionally sized and shaped toengage with some cooperating portion of projectile 600 in such a mannerthat the cooperating portion of projectile 600 may be guided by groove500 during launch.

FIGS. 48 and 49 are, respectively, assembled and exploded perspectiveviews of optional full caliber projectile 600. Projectile 600 comprisesforwardly disposed foreshaft means 630, rearwardly disposed piston mean610, and intermedially disposed shaft means 620. Projectile 600advantageously has a forward-of-center balance. Foreshaft 630advantageously has a relatively high linear density, and shaft 620advantageously has a relatively low linear density. Shaft 620 isadvantageously somewhat flexible, especially resiliently flexible. It iswithin the ability of those skilled in the art to determine thedimensions, relative proportions, and material composition andstructuring of shaft 620, foreshaft 630, and piston 610, in order thatthe resulting mass distribution of projectile 600 may result in anoverall balance of projectile 600 that will enhance in-flight stabilityof projectile 600, and in order that shaft 620 may advantageously besufficiently long, light weight, and otherwise so adapted as to serve asan effective primary or supplementary means of applying aerodynamicstabilization to projectile 600 during flight along an externaltrajectory or flight path after launch. Piston 610 comprises a conicalfrustum shell provided with a forward opening preferably cooperatinglysized and shaped to frictionally engage the rearward portion of shaft620 when the rearward portion of shaft 620 is inserted into the forwardopening of piston 610. Foreshaft 630 advantageously has a rearwardlydisposed portion cooperatingly sized and shaped to insert within andfrictionally engage with the forward portion of shaft 620. It will beapparent to those skilled in the art that optional connecting means maybe used to enhance or make permanent the engagement or connectionbetween piston 610 and shaft 620, and additionally or alternatively, toenhance or make permanent the engagement or connection between foreshaft630 and shaft 620. Piston 610, shaft 620, and foreshaft 630 areadvantageously so adapted as to be substantially coaxially aligned whenmutually engaged or mutually connected as a unit to form projectile 600.

FIG. 50 is a side elevational view of blowgun 110 with optionalprojectile 600 loaded inside bore 120-4 near breech 120-2, with thecooperating portion of projectile 600 resting in and engaged with groove500. FIG. 51 is a sectional view along section line 51-51 from FIG. 50,somewhat enlarged to show in greater detail and clarity the cooperatingportion of projectile 600 resting in and engaged with groove 500, andthe cross-sectional shape of groove 500. It will be apparent to thoseskilled in the art that other cross-sectional shapes are possible forgroove 500. It is within the ability of those skilled in the art todetermine various cross-sectional shape and dimensions that will enableone or more portions of groove 500 to engage one or more cooperatingportions of projectile 600 in order that groove 500 may thereby applyeffective correctional guidance to one or more portions of projectile600 during launch.

FIGS. 47-51, continued. Bore 120-4 is provided with elongate, preferablysubstantially straight groove 500 disposed in the inner surface of bore120-4, with groove 500 preferably aligned substantially parallel to thelongitudinal axis of bore 120-4, and with one end of groove 500terminating open-endedly at muzzle opening 120-6 of bore 120-4, and withthe other end of groove 500 terminating within a predetermined proximityof breech opening 120-2 of bore 120-4, with the distance of theaforementioned proximity to breech opening 120-2 preferably beingsomewhat less than the length of optional full caliber projectile 600,and groove 500 being advantageously further adapted to receive andslidingly engage a cooperating portion of projectile 600 in such amanner that the cooperating portion of projectile 600 may be guidedalong groove 500 in a predetermined path defined by one or more portionsof the surfaces of groove 500, in such a manner that the cooperatingportion or portions of projectile 600 may be guided by the cooperatingportion or portions of groove 500 along a substantially straight linepath which preferably is substantially parallel to the longitudinal axisof bore 120-4, whereby the cooperating portion or portions of projectile600 may move through bore 120-4 with decreased tendency towards tipping,in-bore balloting, and other internal ballistic path and orientationdispersions, and whereby projectile 600 may be launched with improvedinternal ballistic stability and improved consistency.

Additional comments regarding the embodiment depicted in FIGS. 44-46 andsuggestions about related alternative embodiments

It will be apparent to one skilled in the art that by decreasing thediameter of the inner opening of ring-shaped or doughnut-shaped magnet210, it would be possible in certain embodiments to position magnet 210directly against or sufficiently near breech opening 120-2 of barrel 120so that the one or more portions of magnet 210 itself would essentiallydefine one or more portions of an annular shoulder adapted to abbutinglyengage sabot 170, in order that magnet 210 itself might servedouble-duty as both projectile detent 210 and sabot detent 220, or inother words as detent 200. It will also be apparent that in certainembodiments magnet 210 may be shaped and otherwise so adapted as toalso, or alternatively, serve as a mouthpiece. Alternatively, ifembodied as a sufficiently small yet powerful tubular or sleeve-shapedmagnet, magnet 210 could be inserted inside bore 120-4 and theretoaffixed, preferably near breech 120-2, in order that one or moreportions of magnet 210 would thereby essentially provide or define oneor more portions of an internally mounted annular shoulder to servedouble-duty as both sabot detent 220 and projectile detent 210, or inother words as a single-element detent 200. In certain embodiments, acrossbar detent may itself be a magnet or be magnetized by contact witha separate magnet. In certain embodiments, a crossbar orforwardly-extending protrusion affixed to or integral with the crossbarmay be adapted to insert through an opening pierced longitudinallythrough the sabot, so that the crossbar or crossbar extension maythereby directly engage mechanically or magnetically or in othersuitable manner with some portion of the subcaliber projectile. Incertain such embodiments in which the subcaliber projectile is elongateand held in a loaded position at an angle to the longitudinal axis ofthe barrel bore, the crossbar or extension or both may advantageously behinged or flexible or rotatably mounted in such a manner as to be ableto pivot or yield to allow the subcaliber projectile and sabot todisengage smoothly with minimal resistance at the commencement oflaunch. In certain such embodiments, such a crossbar extension may even,for example, extend through a suitably adapted sabot, and within andthrough a hollow shaft, to engage some portion of a suitably adaptedforeshaft, or other appropriate cooperating portion of the projectile.Alternatively, in certain embodiments the sabot may be provided with ahollow inward portion communicating between openings in the front andrear ends of the sabot, with a portion of the hollow portionadvantageously forming a forwardly facing socket in the forward end ofthe sabot, so that when the projectile is engaged with the sabot, arearward portion of the projectile protrudes into and through thehollowed sabot portion and extends therethrough rearwardly past the rearend of the sabot so that some portion or portions of the rearwardlyprotruding projectile rear portion may engage with one or morecooperating portions of an appropriately adapted projectile detent.

In a possible alternative embodiment of the BB shot-launching sabotblowgun illustrated in FIGS. 44-46, the magnetic detent may bepositioned along the barrel between the sabot detent and the muzzle endof the barrel, and so positioned and oriented as to attract and hold theBB shot in place against the inner surface of the barrel bore, oralternatively in certain embodiments to possibly hold the BB shot inplace against the inner surface of some forwardly extending rim of thesabot. When considering certain embodiments it is apparent that it maynot be necessary that the BB shot and sabot should be in direct abuttingcontact prior to the commencement of launching acceleration. Rather, aslong as the BB shot and an appropriately adapted sabot (such as the foamcylinder sabot illustrated in FIGS. 44-46) are confined withinreasonable proximity to each other, at the commencement of launchingacceleration the sabot may move forward to engage the BB shot andthereupon assume the abutting relationship with the BB shot which allowsthe sabot to efficiently transmit thrust to the BB shot. It also may notbe necessary in certain embodiments for the sabot to be in directcontact with the sabot detent prior to the commencement of launchacceleration. In such embodiments the sabot detent may possibly merelyserve to prevent or resist further breechward movement of the sabot inthe event that the sabot happens to move rearward far enough to come incontact with the sabot detent, and the sabot detent may also possiblyserve double-duty as an anti-inhalation safety means to prevent thepreferably lightweight sabot from being sucked out the breech by theuser. Again, the type of foam cylinder sabot illustrated in FIGS. 44-46is one type of sabot appropriate for such embodiments, since such a foamcylinder sabot may simply rest in place on top of the inner surface ofthe bore, especially if the bore is oriented substantially horizontally.In fact, such an embodiment may be entirely functional without a sabotdetent, however inclusion of the sabot detent may still be advantageousin that the detent may also may serve double duty as either a primary orredundant anti-inhalation safety means to prevent the lightweight sabotfrom being sucked out the breech by the user. Also, in certainembodiments it may be advantageous to keep the BB shot and the sabot indirect abutting contact while in loaded position up until launch, inorder, for example, to reduce any tendency of a compressible foam sabotto ride up over or past the BB shot during launch.

BB-launching sabot projectile blowguns may also be adapted to bebreechloading rather than muzzle-loading, as will be apparent to oneskilled in the art after having reviewed FIGS. 22-43 with theiraccompanying descriptions.

It will be apparent to one skilled in the art that the embodimentdepicted in FIGS. 44-46 may be used as a basis for alternativeembodiments suitable for launching various types and sizes of sphericalprojectiles, or other substantially non-elongate projectiles, other thanBB-shot.

It will be apparent to one skilled in the art that in addition to thetype of foam cylinder sabot described above, there are numerousalternative sabot embodiments suitable for use as sabots with BB shotand with other types of spherical or non-elongate projectiles, as wellas with other types of projectiles. However, the type of foam cylindersabot described above is particularly well-suited for application to ado-it-yourself kit because such foam sabots can be easily formed or madeby the user according to the method described below.

Following is a description of a method of creating or forming the foamcylinder sabots for use in certain embodiments of the BB launching sabotblowgun, which is particularly well-suited for application to ado-it-yourself kit embodiment. In this method, the user uses a handheld,approximately quarter-inch hole punch, of the type commonly used inoffices and schools, and which often operates in a manner similar topliers. It may be necessary to modify the hole punch to allow it to openwider than is typical for use in punching paper. Some commerciallymanufactured hole punches are already available that allow wider openingof the jaws. The user may insert between the jaws of the hole punch astrip or sheet of preferably open cell rubber or plastic foam, with thefoam strip or sheet preferably about 0.5 inch (one-half inch) thick(more or less), and then use the hole punch to punch a hole in the foamsheet. The foam will compress as the punch squeezes down, and after thepunch action is completed, the cylinder-shaped piece of foam that waspunched out should quickly spring back to shape from its temporarycompression. A relatively easy-to-find source of such foam isself-adhesive foam weatherstripping seal; since such strips ofweatherstripping foam typically have a removeable paper or film backingover a sticky self-adhesive side, the user can either leave the backingin place, or else replace the backing with a replacement layer of adifferent kind of paper, plastic, foam, or the like. The thin sheets offlexible craft foam, sold in hobby and craft stores, are one example ofa type of suitable replacement layer material. The user may peel thebacking off of a strip of the weatherstripping foam, apply the stickyside of the strip to a piece of the thin craft foam, and then use thehole punch to punch out one or more cylinders from the resultingcomposite foam sheet. It would also be possible to make larger holepunch tools, similar to the ones used for scrapbooking crafts, etc, thatwould punch out several foam cylinders with every punch action. It willbe appreciated that a suitable barrel tube for the blowgun should bechosen so that the tube's inner diameter or bore caliber will be a goodmatch, although preferably not too snug, for the foam cylinders producedby the hole punch. Or alternatively a hole punch of a suitably matchingsize for a particular bore caliber could be found or manufactured.

As was mentioned above, other types of sabots besides the foam cylindersabots may be used with a BB shot projectile. One example of such analternate type of sabot, that is still reasonably easy for a user tomake by hand, is a conical shell sabot, sized at the base tosubstantially slidingly seal with the barrel bore, and truncatedsufficiently near the tip to leave a forward opening somewhat smaller indiameter than the diameter of the BB. The BB may be partially insertedinto the forward opening of such a truncated sabot cone to engage theannular shoulder defined by the rim of the opening. The fit of such atruncated conical sabot may possibly or more easily be made somewhatmore precise or snug in the bore than with the foam cylinder sabot,since there would be a smaller area of surface contact (and accordinglyreduced friction) with the cone than with the cylinder. This possiblymore precise fit and smaller area of surface contact may in turn yieldhigher velocities, although such a conical shell sabot may be more timeconsuming to make by hand than the foam cylinder sabots described above.Incidentally, such a truncated conical shell may alternatively be gluedto or otherwise affixed to a BB shot as a convenient way to make a fullcaliber projectile. It will be apparent to one skilled in the art thatfoam cylinder sabots or truncated conical shell sabots may easily besized and shaped to use with subcaliber spherical projectiles of sizesother than BB shot sizes, and that both types of sabots, or suitableequivalents, as well as many other alternative types of sabots, may becommercially or mechanically manufactured rather than being made by handby the user.

Additional descriptions of and notes on some alternative embodiments:The detailed descriptions above, accompanying FIGS. 1-43, containcomments that suggest or briefly describe some possible alternativeembodiments of my invention. The principles of my invention will alsosuggest or make apparent to one skilled in the art numerous otheralternate embodiments of my invention. Following are additionaldescriptions and suggestions of illustrative examples of some possiblealternative embodiments of the invention.

The embodiment of sabot detent means 220, as described in the embodimentdepicted in FIGS. 22-43, is well adapted to enable the embodiment of myinvention depicted in FIGS. 22-43 to function effectively as abreech-loader. It will be apparent to one skilled in the art that theembodiment described and depicted in FIGS. 22-43 could also oralternatively be used as a muzzle loader, if necessary using a ramrod orweight on a string or other suitable means to push sabot projectileassembly 190 backwards down bore 120-4 from muzzle 120-6 until sabot 170engages sabot detent 220. Some alternative embodiments of my inventioncould be intended for use strictly as muzzle-loaders, in which case anyprotrusions comprised by sabot detent 220 might possibly extend furthertrans-versely across, or even completely transversely across, bore 120-4or breech 120-2, such as, for example, one or more narrow transversecrossbars, or a mesh screen, affixed across breech 120-2. Furthermore,the embodiment depicted in FIGS. 1-21 may also, if desired, be operatedas a muzzle loader.

In the embodiment described and depicted in FIGS. 22-43, theillustrations depicted sabot detent 220 as comprising a single narrowramp-like protrusion 220, affixed to or integral with and radiallyextending from the inner surface of bore 120-4 at or near breech 120-2,in such a manner that detent extension 220 is aligned lengthwisesubstantially parallel to the longitudinal axis of bore 120-4, with asloped surface facing rearwards toward breech 120-2, and a shouldersurface facing forward towards muzzle 120-6. It will be apparent to oneskilled in the art that sabot detent 220 might alternatively comprise aplurality of such ramp-like protrusions, or that each such of one ormore protrusions or extensions might be shaped somewhat differently thanthe ramp-like form depicted in FIGS. 22-43, or that the shape,alignment, positioning, and orientation of any such protrusions orextensions might also be different than that specifically shown in FIGS.22-43. It will further be apparent to one skilled in the art that thereare numerous suitable alternative embodiments for sabot detent 220.

It will also be apparent to one skilled in the art that alternativeembodiments are possible in which sabot detent 220 engages sabot 170frictionally, or compressively, or both, rather than abuttingly. Forinstance, an example of such a type of alternative embodiment mightcomprise elements identical to those of the embodiment depicted in FIGS.22-43, with the exception that sabot detent 220 would instead comprise aportion of bore 120-4, preferably near or at breech 120-2, that has beentextured, or essentially slightly reduced in caliber, or both, in orderto engage sabot 170 with an enhanced frictional grip, or a mild forcefit, or both. Some such embodiments, that might possibly utilize one ormore protrusions or extensions protruding inwardly from the innersurface of bore 120-4 in order to provide a section of essentiallyreduced caliber, could be used as either an abutting sabot detent 220,or as a frictional/compressive sabot detent 220, depending merely onmethod of use, or in other words depending on whether the user insertedthe sabot into and partially through, but not past, the reduced calibersection (frictional/compressive), or else inserted the sabot completelythrough and past the reduced caliber section (abutting). Any such sabotdetent 220, comprising bore sections that are textured or essentiallynarrowed or both, preferably near or at the breech, could be used toprovide alternative embodiments that may be used either withoutprojectile detent 210, in essentially the manner depicted in FIGS. 1-21,or alternatively with projectile detent 210, in essentially the mannerdescribed and depicted in FIGS. 22-43.

It will be further apparent to one skilled in the art that alternativeembodiments are possible in which detent means 200 comprises projectiledetent 210 but does not comprise sabot detent 220. One example of suchan alternative embodiment is one in which sabot cone 170 is sized andshaped at its base to frictionally engage the unaltered, or in otherwords untextured and unreduced in caliber, surface of bore 120-4 withsufficient snugness to resist or prevent axial displacement of sabot 170towards or out breech 120-2 when sabot 170 is loaded within bore 120-4of barrel 120 prior to launch acceleration. It will be recognized thatthis is similar to the method of securing sabot 170 used in theembodiment illustrated in FIGS. 1-21, but that the degree of frictionalengagement between sabot 170 and bore 120-4 would, in such analternative embodiment, preferably be sufficiently strong not only toprevent or resist breechward displacement of loaded sabot projectileassembly 190 due to gravity, but also to prevent or resist breechwarddisplacement of sabot projectile assembly 190 due to any magneticbackpressure possibly imposed by magnetic projectile detent 210, as wasdescribed above, or other possible backpressure due to other causes suchas a possible spring tension bias due to the possible flexing of shaft160 in embodiments in which shaft 160 is resiliently flexible.

It will also be apparent to one skilled in the art that alternativeembodiments are possible in which blowgun 110 does not comprise detentmeans 200, or in other words comprises neither projectile detent 210 norsabot detent 220. One such example was described and depicted in FIGS.1-21. However, it will be apparent to one skilled in the art thatalternative embodiments are possible which do not comprise detent means200 and also, unlike the embodiment depicted in FIGS. 1-21, do notrequire the user to keep barrel 120 uptilted with muzzle 120-6 higherthan breech 120-2. An example of such an embodiment could be obtained bytaking the elements of the embodiment depicted in FIGS. 1-21 andreplacing conical shell sabot 170 with a sabot comprising a lightweightfoam cylinder sized to substantially match the caliber of bore 120-4. Insuch an embodiment, premature or excessive lateral or transversedislocation of cylindrical sabot 170 relative subcaliber projectile 140may be substantially prevented by the transverse travel limits imposedby the transverse dimensions of bore 120-4. Furthermore, in such anembodiment, sabot 170 and projectile 140, even if not continuouslyabuttingly engaged after loading insertion and prior to launchacceleration, could assume such an abutting engagement as launchacceleration commenced, provided they remained within reasonableproximity of one another prior to launch acceleration. Such acylindrical sabot could be composed of either a relatively flexible,compressible foam such as foam rubber, or alternatively of a relativelyrigid molded plastic foam. (Other suitable materials will be apparent toone skilled in the art. Also apparent to one skilled in the art will bealternate sabot embodiments such as, for example, a hollow or partiallyhollow cylindrical shell open at either the forward end or the rear end;or if open at both ends, with a transverse inner partition locatedsomewhere between the two ends.)

If compressible, such a cylindrical sabot 170 could be transverselysized so as to fit bore 120-4 slightly snugly. Whether slightly snug,slightly loose, or neither snug nor loose within bore 120-4, foamcylinder sabot 170 may have considerable resistance to prematuredisplacement after loading, due to its relatively light weight, possiblysomewhat rough texture, and fairly large amount of surface area incontact with the inner surface of bore 120-4. An elongate embodiment ofprojectile 140 would generally have less resistance than cylinder sabot170 to premature displacement due to projectile 140 typically beingembodied in a slender, smooth, slick-surfaced form. Yet, when bore 120-4is leveled horizontally, projectile 140, of essentially the elongatetype illustrated in FIGS. 1-43 above, would rest upon the inner surfaceof bore 120-4 without sliding, and would perhaps resist sliding even ifbore 120-4 were to be slightly down-tilted, with muzzle 120-6 slightlybelow the level of breech 120-2, at angles still fairly close tohorizontal (in such embodiments it may be advantageous for any foreshaftportion of the projectile not to be wider than the shaft portion, inorder that as much of the length of the projectile as possible might bein direct contact and direct frictional engagement with the bore's innersurface). Furthermore, in embodiments in which cylinder sabot 170 fitssufficiently snugly within bore 120-4, sabot 170 could support itselfand projectile 140 when barrel bore 120-4 is uptilted with muzzle 120-6higher than breech 120-2, according to the essential method of usedepicted in FIGS. 1-21. Accordingly, in such an embodiment, the usermight possibly be able to orient blowgun 110 with barrel bore 120-4up-tilted, horizontal, or perhaps even slightly down-tilted with muzzle120-6 slightly below breech 120-2, without causing excessive prematuredisplacement of sabot 170 and projectile 140, provided any manualhandling and reorientation of blowgun 110 was sufficiently gradual andsmooth. However, it will readily be appreciated that such an embodimentwould very likely require relatively delicate and limited handling andmaneuvering, and would probably be limited in situations in which itwould be suitable for use, and to users with sufficient skill for suchcareful and controlled handling, when compared to the more flexibleembodiment depicted in FIGS. 22-43. A similar embodiment, operatingwithout detent means 200 and without up-tilted barrel, yet using anon-elongate projectile, could, for instance, use a foam cylinder sabotin cooperation with an essentially spherical projectile that has beenprovided with one or flattened facets upon which the projectile may restupon the bore without rolling. Extensions or protrusions affixed to orintegral with an elongate or non-elongate projectile, such as varioustypes of fletching, may help to increase the projectile's resistance toprematurely sliding along and through the barrel bore when the barrelbore is tilted away from the horizontal.

It should be noted that some types of extensions or protrusions affixedto or integral with the subcaliber projectile, such as, for example,fletching or vanes similar to those used on archery arrows or throwingdarts, could at the vanes' or extensions' lateral extremities or extremelateral surfaces be substantially full-caliber; however, the frontalprofile of a subcaliber projectile that included vanes with lateraledges substantially full caliber would still have a smaller area thanthe frontal profile of a full caliber projectile with an affixed orintegral full caliber piston, and therefore could still be considered asa type of essentially subcaliber projectile. One or more flexible(preferably limply flexible) extensions, such as string or hingedfingers, could be affixed to or integral with a subcaliber projectile insuch a manner as to allow the user to engage the sabot rearwardlyagainst the projectile, draw the flexible extension/s tautly back andpast the outer edge or edges of the full caliber portion of the sabot,and then insert the sabot projectile assembly thus formed into the boreso that the projectile's flexible extensions are pinched between theouter edge of the sabot and the inner surface of the bore, therebycreating a mild force fit or compression, with the pinched portions ofthe flexible extensions temporarily creating a sort of full caliberportion of the otherwise essentially subcaliber projectile. After launchacceleration and exit from the bore, any such flexible extensions wouldbe released from being pinched between bore and sabot, with the sabotthen being free to discard, and the flexible extensions free to swing toa position of reduced air resistance, trailing behind the main portionof the projectile.

Yet another example of an alternative embodiment which does not comprisedetent means 200 and does not require the user to keep barrel 120uptilted with muzzle 120-6 higher than breech 120-2, is one in whichsabot 170 comprises a loosely formed fibrous mass, such as, for example,a wad of kapok fibers, or of polyester fibers, cupped around the rearend of shaft 160 and squeezed or force-fitted inside bore 120-4, so thatradial compression imposed by bore 120-4 upon such a fibrous mass sabot170 keeps sabot 170 gripped firmly in place by the inner surface of bore120-4, and radial compression transmitted by such a fibrous mass sabot170 to shaft 160 or other portion of projectile 140 in turn keepsprojectile 140 gripped firmly in place by fibrous mass sabot 170. Aslightly different version of such an embodiment could employ more thanone fibrous mass, allowing some portion of subcaliber projectile 140 tobe sandwiched between two or more fibrous masses, with additionalfibrous masses used behind, if necessary, to form a pusher plug sabotcomponent. It will readily be appreciated that such embodiments thatrely on radial compression must be carefully calibrated to avoid anexcessively snug force-fit of sabot 170 within bore 120-4 such as wouldimpose too much launching resistance to be readily overcome by thebreath of the user.

Furthermore, any such embodiments that use fibrous masses in the sabotmeans should preferably be used in cooperation with smooth contactsurfaces on subcaliber projectile 140, since any rough projectilesurfaces that could snag sabot fibers could accordingly cause failure ofsabot 170 to discard cleanly, if at all. To ameliorate the risk of fibersnags, a smooth layer of paper, plastic, cloth, or foam could be gluedto some portion of the fibrous mass to act as a snag-preventinginterface with projectile 140. Alternatively, the fibrous mass or massescould be entirely replaced with one or more sections of a material suchas compressible foam. Alternatively, cooperating sections of molded foamor plastic or other suitable material could be more precisely formed tocooperate with bore 120-4 and with some portions of projectile 140 inorder to provide a slightly compressible or resiliently compressiblesandwich carrier means for projectile 140. In order to provide adequateforce-fit or radial compression, without unduly increasing the snugnessof any sabot force-fit within bore 120-4, and any correspondinglyincreasing launching resistance, any such sandwich carrier sabotportions might be shaped so that compression would be applied by bore120-4 only to limited portions of the carrier structure, and possiblyalso so that any such compressible or resiliently compressible portionswould be able to move somewhat independently of non-compressed portionsof the carrier structure, and possibly also so that the compressible orresiliently compressible portions would be provided with members orprotrusions that would cooperate with indentations or notches inprojectile 140 in order to help to lock projectile 140 in positionrelative the carrier sections as long as compression was applied. Anysuch sandwich carrier sabot components may optionally be provided withintermediary connecting members connecting the carrier sections to eachother, or to an optional pusher plug component, or both. A somewhatdifferent, yet related type of embodiment which utilizes mildcompression, could include one or more sabot sections, which rather thanfunctioning as carriers to support a portion of the projectile off ofthe bore's inner surface, would instead function as compression orrestraining members to hold a portion of the projectile directly againstthe bore's inner surface, so that the sabot portion or portions are ineffect fitted or squeezed side-by-side with a portion of the projectilewithin the bore, preferably snugly enough to resist or prevent prematuredisplacement along the bore. Such an embodiment might benefit from anoptional pusher plug structure rearwardly affixed to or integral withthe compression portion of the sabot, with the pusher plug structureadapted to abuttingly engage some rearward-facing portion of thesubcaliber projectile.

It should be noted that non-elongate projectiles, particularly sphericalprojectiles, may be used as subcaliber projectiles. One basic way toprovide a sabot for a spherical projectile or other non-elongateprojectile is to use a conical shell sabot sized at the base tosubstantially sliding seal with the barrel bore, with the conical shelltruncated sufficiently near the tip to leave a forward opening somewhatsmaller in diameter than the diameter of the spherical projectile,thereby making what we may term as a frustum shell sabot. The sphericalprojectile may be partially inserted into the forward opening of such afrustum shell sabot to abuttingly engage the annular shoulder defined bythe rim of the forward opening.

Launching spherical or other non-elongate projectiles from a blowgunthat was initially designed or adjusted to launch elongate projectilessuggests other general possibilities for alternative embodiments of myinvention. When using, modifying, or designing a blowgun that wasinitially adapted to launch sabot projectile assemblies of a givenlength, should the user or designer wish to launch sabot projectileassemblies in which the projectile proper has a shorter length than thatof one of the original projectiles for which the blowgun was initiallyadapted or adjusted, the user or designer has at least two optionsavailable: A first option is to use a sabot substantially the samelength as the original sabot, with a resulting shorter total length ofthe sabot projectile assembly, and to accordingly adjust (shorten) thedistance between the projectile detent and the sabot detent until thedistance is sufficiently short to provide secure confinement of theshortened sabot projectile assembly. A second option is to use a longersabot so that the total length of the sabot projectile assembly is stillthe same as, or close enough to, the length of the original sabotprojectile assembly, to thereby allow the use of the original distancebetween the detent elements. Such a lengthened sabot could, for example,be simply a frustum or conical shell of lengthened proportions, orcould, for example, be a relatively short main conical or frustum bodywith a forwardly extending, fairly rigid member. An illustrative,non-limiting example is a section of approximately quarter-inch sodastraw forwardly affixed to a conical shell, so that the rim of theforward opening of the straw could abbutingly engage a three-eights inchdiameter spherical projectile in order to launch it as a subcaliberprojectile from a 62 caliber barrel bore. It should be noted that itwould not be strictly necessary for the soda straw section to be affixedto the forward end of the conical shell; the mutual opposition of theprojectile and sabot cone imposed by the antagonistic detent means couldkeep the soda straw section sandwiched between the projectile and thesabot while in loaded position, in which case the sabot cone and strawsection would be free to separate from each other as well as from theprojectile after exiting from the muzzle at the conclusion of launchacceleration. It will be apparent to one skilled in the art that manyalternative embodiments are possible which follow the essential spiritof this illustrative example, without specifically using a conical shelland a tubular soda straw section, and it will be further apparent thatalternative embodiments of sabot size, or detent positioning, or both,are possible which are intended to adjust for longer total length of thesabot projectile assembly, rather than for shorter total length of thesame.

Furthermore, if a user or designer wishes to launch sabot projectileassemblies that are either shorter or longer than the length of theoriginal sabot projectile assembly the blowgun was initially adapted oradjusted to launch, it will be apparent to one skilled in the art thatembodiments are possible in which the detent means is further soadapted, or further comprises suitable connecting means so adapted, asto allow the projectile detent or sabot detent or both to able to berepositioned and/or re-oriented relative each other and the bore, andpossibly reaffixed or re-secured in each new position and orientation,in order to accommodate and securely hold sabot projectile assemblies ofvarying lengths. Such detent connecting means might possibly beadjustable in either continuous or incremental fashion. Such ability toadjust positioning and orientation of detent elements also make itpossible to accommodate projectiles in which the magneticallyattractable projectile portion is dimensioned, or positioned within theprojectile, differently than the positioning or orientation of such aportion within the original projectile the blowgun was initially adaptedor adjusted to launch. Furthermore, such ability to adjust positioningand orientation of detent elements also make it possible to makeadjustments to blowgun performance, such as initial launchingresistance, according to user preference and ability, which vary fromindividual to individual, and which may change over time within the sameindividual due to the effects of training and practice or adoption ofnew techniques or methods of use.

Some additional notes on certain advantages, alternate embodiments, andmethods of use

In general, my invention provides a blowgun and associated projectileswhich display improved performance in terms of range, trajectory,accuracy, velocity, and convenience and economy of use.

Some specific advantages and performance improvements, and certainalternative embodiments or suitable methods of use, provided by or madepossible by my invention may include:

*In certain embodiments, use of the associated detent means has theadditional effect of increasing consistency from shot to shot, thusimproving accuracy potential.

*In certain embodiments, there may be a boost in exit velocities due toa slight but substantial delay effect, imposed by the associated detentmeans, which allows higher thrust pressures or earlier peak pressures todevelop during launch acceleration.

*In addition to launching subcaliber projectiles, with certainembodiments of my invention the user may, with little or no adjustment,still use the blowgun to launch various types of full caliberprojectiles. Furthermore, due to the detent delay effect mentionedabove, exit velocities obtained with the full caliber projectiles may insome cases be higher than those obtained shooting the same full caliberprojectiles from an otherwise comparable prior-art blowgun, and if thefull caliber projectile is appropriately adapted, accuracy and stabilitymay also be improved.

*By removing the constraint that a portion of the projectile proper mustserve as a full caliber piston, my invention introduces much greaterfreedom in designing the projectile so as to adjust or modify itsproperties such as form factor, mass, mass distribution, andconfiguration of aerodynamic surfaces in order to optimize one or moreperformance characteristics such as aerodynamic properties, accuracy,balance, stability, target penetration, and transfer of energy to thetarget. This freedom gives the user or designer much greater control intailoring the performance of a projectile for any of a great variety ofspecific applications and methods of use.

*My invention provides a number of specific exemplary subcaliberprojectiles appropriate for use with the improved blowgun, and inparticular a type of exceptionally streamlined subcaliber projectilewhich exhibits highly advantageous aerodynamic properties and balancecharacteristics which result in improved ballistic coefficient,increased range, flatter trajectories, improved stability and accuracy,while also providing better target penetration.

*My invention further provides an example of such a type of subcaliberprojectile which may have a substantially longitudinally elongate areaof surface contact with the barrel bore during launch acceleration, andwhich therefore additionally exhibits improved stability as it traversesthe barrel bore under acceleration and in which such improved internalballistic properties may in turn yield consequently improved stabilityand accuracy as the projectile travels along its external trajectory.The principle may also be applied to provide a full caliber projectilewith improved internal ballistic stability. It may be noted that due tothe limited ranges at which prior-art blowguns are effective, accuracyproblems caused by internal ballistic shortcomings may not have been asnoticeable, or may have been considered to be within acceptable limits.However, at the extended ranges made possible by my invention, itbecomes more significantly advantageous to reduce even small deviationsor inconsistencies which would be more noticeably amplified over longerranges.

*In some embodiments, my invention provides an alternative orcomplementary strategy for improving internal ballistic guidance andstability of the projectile, by using a barrel provided with one or moresubstantially straight, longitudinal grooves or protrusions of the borethat are substantially parallel to the longitudinal axis of the bore andwhich cooperate with the projectile or projectile assembly to providemore precise guidance to the projectile or sabot projectile during itstravel through the bore. Thus, certain embodiments of my invention makeit possible to apply improved, more precise internal ballisticcorrectional guidance to the sabot projectile assembly as it travelsthrough the bore during launch acceleration, which in turn providesgreater stability and accuracy as the projectile travels along itsexternal trajectory.

*Thus, certain embodiments of my invention may achieve such improvedinternal ballistic guidance and stability of the projectile in at leasttwo possible different ways, as were just precedingly described, andwhich may be used either independently or conjointly, as described inmore detail elsewhere.

-   -   *Certain embodiments of my invention, particularly embodiments        which include longitudinal bore grooves or bore protrusions, may        make it possible to reduce the area of bearing surface in        contact between bore and projectile or projectile assembly.

*Sabot projectile components, consistent with prior-art shootingtradition, and advantageously for the convenience and economy of theuser, may in certain embodiments of my invention be so adapted as to becompletely reusable and thus after launching may be retrieved andre-launched again and again, particularly in target shooting.

*My invention, in certain embodiments, provides a type of target andassociated method of target shooting highly suitable for use with theassociated subcaliber projectiles, and which offers a wider variety ofshooting methods or experiences to the user. Furthermore, the type oftarget and the method of shooting provided by certain embodiments makeit possible for the user to substantially reduce the potential fordamage to projectiles caused by impact with the target as well as byimpact with other projectiles either already lodged in the target orsubsequently launched at the target. Also greatly reduced is the timeand effort, as well as the potential for damage to projectiles,associated with the process of retrieving the projectiles from thetarget. In brief, such a target may include a shoot-through target facewhich is adapted to be completely penetrated by the projectile. At asuitable distance, preferably somewhat greater than the length of theprojectile, behind the target face, may be positioned a yielding,flexible or moveable backstop which may dissipate the impact of the dartwithout being penetrated, allowing the spent dart to either drop beneaththe target assembly to an external collecting area, or else drop to acollecting area or structure contained within or built into the targetassembly itself. Projectiles used with such a target typically have asubstantially blunt forward end.

*In many embodiments, my invention may achieve its functions withoutrequiring any increase in snugness of fit, and requiring negligible, ifany, increase in friction, between the barrel bore and the sabotprojectile, when compared to the friction and snugness of fit betweenthe barrel bore and a prior-art full-caliber projectile. Thus, usingmany embodiments of the improved blowgun and associated projectilesprovided by my invention, a subcaliber projectile may be launched witheither negligible or no loss of propulsive efficiency and accuracy incomparison to the propulsive efficiency and accuracy of a prior-artblowgun using full caliber projectiles. As will be seen, in certainembodiments my invention actually achieves improved propulsiveefficiency, improved accuracy, or both, as compared to prior-artperformance. Particularly, due to the flatter trajectories made possibleby using subcaliber projectiles, most or all embodiments of my inventionmay be considered to achieve improved accuracy in the sense of providingimproved ease in aiming, due to reduction in the amount of elevationcompensation required when aiming, particularly at extended ranges.Furthermore, many embodiments also offer additional accuracyimprovements in terms of consistency of shot placement due to improvedstability and consistency of projectile launch and flight.

*My invention generally achieves its functions and advantages throughstrategies or principles that operate independently of, and yetcompatibly with, prior-art strategies or solutions for improving blowgunperformance in terms of launching a projectile or projectile assembly ofa given mass with improved velocity and accuracy. Thus, in addition tobeing used to provide a complete set including a blowgun with associatedsabot projectiles, along with, if so desired, an associated targetparticularly suited for use with the blowgun and projectiles, myinvention may alternatively be used to provide stand-alone solutionssuch as projectiles, sabots, kits, accessories, and targets that wouldallow a user, for example, to convert a pre-existing blowgun to launchsubcaliber projectiles, or to build or assemble from scratch his or herown subcaliber blowgun, or to use pre-existing full caliber projectilesas subcaliber projectiles in a blowgun of larger bore caliber, or, forexample, to allow resupply, repair, and maintenance of any of thecomplete or partial sets, or any of the stand-alone solutions, describedor suggested above. It is accordingly desired that protection beprovided both to complete sets, to partial sets, and to stand-alonesolutions provided by my invention according to its details, spirit, orprinciples.

*Certain embodiments of my invention may be provided with more than onebarrel or barrel bore. In certain such embodiments, one of the includedbores may have a larger caliber than the caliber of another of theincluded bores, thereby allowing the user the option to either launch aprojectile as a full caliber projectile from the smaller caliber bore,or to launch the same or identical projectile, with the help of anappropriately adapted sabot means, as a subcaliber projectile from thelarger caliber bore.

*Certain principles of my invention may be used to provide improved fullcaliber projectiles, that exhibit, for example, improved balance, orincreased ease of retrieval from a target, or to launch full caliberprojectiles with improved inner ballistic guidance and stability.Improved target designs and strategies provided by my invention forreducing damage to projectiles may be applied to either subcaliberprojectiles or full caliber projectiles. It is accordingly desired thatprotection be provided both to complete sets, to partial sets, and tostand-alone solutions that use such principles.

*It will be apparent to one skilled in the art that my invention alsomakes it possible to efficiently simultaneously launch a plurality ofsubcaliber projectiles.

*The principles of my invention may be applied not only to blowguns, butalso, for example, to improve the performance and extend the possibleuses of paintball guns and many other types of projectile launchingdevices. An example is the use of the sabot to transmit rifling spinfrom a rifled barrel without rupturing the paintball, which hadpreviously prevented the use of grooved barrel rifling in paintballguns. Also, paintballs may be re-shaped or otherwise adapted to functionas frangible elongate subcaliber projectiles, with suitable affixedstabilizer portion, for launch from my invention. My invention couldalso be adapted to launch non-frangible subcaliber projectiles fromdevices other than blowguns, even including firearms or artillery.

*My invention's use, in certain embodiments, of discarding sabots withsubcaliber projectiles makes it possible for the subcaliber projectileto engage the sabot asymmetrically, or in other words to engage thesabot at some point or region other than the region at and near, oressentially concentric to, the axial center of the sabot, or center ofthe front end of the sabot, without adversely affecting the aerodynamicperformance or accuracy of the subcaliber projectile proper after sabotdiscarding occurs. My invention's use, in certain embodiments, ofdiscarding sabots with subcaliber projectiles also makes it possible touse bores and correspondingly shaped and sized sabots whosecross-sectional shape is other than essentially that of a circular disk,without adversely affecting the aerodynamic performance or accuracy ofthe subcaliber projectile proper. Possible examples of othercross-sectional bore shapes, and matching cross-sectional sabot shapes,might include polygons or other plane closed figures, which could beeither symmetrical or assymetrical. Such a bore might allow a variety ofnew construction techniques and materials for barrels, bores and sabots.Such a bore might also be so shaped that the cross-sectional shape ineffect rotates upon the bore axis along the transition from breech endto muzzle end, with each point on the perimeter of the cross-sectionalshape describing a helical path from breech end to muzzle end, in orderto provide the essential effect of barrel rifling. Another example is ahorseshoe-shaped or u-shaped cross-sectional bore, which could be usedto provide a raised track for the projectile to travel upon, pushed by acorrespondingly u-shaped sabot. It will be apparent to one skilled inthe art that similar principles could be applied to provide sabotspre-shaped to engage a particular cross-sectional bore shape oressentially rifled bore, as well as to provide essentially fluted andpossibly rifled surfaces on a preferably subcaliber portion of theprojectile proper that would allow additional aerodynamic correctionalguidance, possibly including aerodynamically induced stabilizing spin,of the projectile in flight.

*Certain embodiments of my invention may allow efficient use of borerifling in the blowgun barrel, generally by using sabots which arepre-graved or pre-shaped to cooperate with the rifled bore with minimallaunch resistance, and to thereby stabilizingly spin pellets andpaintballs, as well as elongate projectiles. Advantageous texturing ofsome portion of sabot, such as an optional projectile engagement socket,as well as urging of the accelerating sabot against the inertial mass ofthe pellet or projectile, may help to provide secure engagement totransmit rotational acceleration applied by barrel rifling.

*Certain embodiments of my invention may improve internal ballisticstability by shaping the sabot asymmetrically, such as, for example,shaping the sabot with a slanted aft surface in order that launch thrustmight consistently bias the sabot towards a certain side of the bore,thus reducing any tendency of the sabot to bounce from side to sidewithin the bore during launch acceleration, which may be possible whenusing sabots with a slightly loose fit within the bore, as is typical ofblowgun projectiles. After sabot discarding occurs, the asymmetricsurface or shape of the sabot will not adversely affect the aerodynamicproperties of the projectile proper.

*In certain embodiments, the bore may be either tapered or flared forsome portion of its length in order to provide either a choke effect ora loosening effect.

*In certain embodiments, positive connecting means may be used to securethe sabot means and the subcaliber projectile together prior to loadingthe sabot projectile assembly into the blowgun barrel bore, to suit userpreference or convenience in handling and loading. However, manyembodiments of my blowgun will still be fully functional in terms oflaunching the associated sabot projectiles without the use of suchconnecting means. When such connecting means are employed, they may bedisengaged during actual launch acceleration or exit, as describedabove, or alternatively, they may be so adapted as to be manually ormechanically disengaged prior to or during the loading process, so thatthe sabot means and subcaliber projectile, while loaded and in batterydisposition prior to launching, have no direct positive connection, butrather a direct abutting connection or direct nestingly abuttingconnection as explained earlier. Parts which lock and unlock by snappingon and off or by twisting on and off are some examples of positiveconnecting means suitable for use in such embodiments. In someembodiments, disengagement of the connecting means may also be actuatedby the resistance of the detent means against the sabot projectileassembly during loading or launch initiation, or by inertial resistanceduring launch initiation. For example, the barrel bore might include ashort rifled section at or near the breech, adapted to engage the sabotand thereby twist the sabot during loading insertion, in order todisengage a threaded (or other type of twist-on/twist-off) connectionbetween the sabot and the projectile. Such a rifling-twisted sabot mightbe easier to use with an optional insertion tool that included a sabotpusher member adapted to rotate independently of a handgrip member.

Certain embodiments which provide a positive connection between thesabot means and the subcaliber projectile may exploit the air pressureof launch thrust to actuate the disengaging of the positive connectionor positive connecting means. For example, an internal, independentlymoving piston or bellows-flap style valve may be housed within the sabotand connected or linked to the positive connecting means or structuresin such a way that the pressure differential supplied by the user'sbreath upon the internal piston or flap valve would provide sufficientforce to displace the piston or flap along with the linked connectingmeans enough to disengage the connection. This type of pressurizeddisengaging actuation would be able to exploit much more total forcethan could be provided by atmospheric drag upon the sabot at typicalblowgun projectile velocities. In some embodiments, use of a positiveconnection between the sabot means and subcaliber projectile, along withsuch means for pressurized disengaging actuation, might allow theblowgun and projectile to function without the use of an external detentto resist premature axial displacement of the sabot projectilecomponents forwardly relative the bore. Alternatively, such a detentmight be used to engage either the subcaliber projectile or the sabotmeans, or both, in order to create a slight delay effect to enhance thefunction of the pressure actuated disengagement mechanism, as well as tosecure the sabot projectile assembly in place within the bore prior tolaunch acceleration. In such embodiments, it may not always be necessaryto use a detent to secure the subcaliber projectile against forwarddisplacement. Rather, the detent might only be needed to secure thesabot means in position within the bore, while the positive connectingmeans might secure the subcaliber projectile to the sabot means. In someembodiments, the inertia of some portion of the sabot projectileassembly or the frictional engagement of the sabot means with the innersurface of the bore might be sufficient, with no need for an externaldetent means, in order to provide the necessary resistance or delay inorder to allow the disengaging mechanism to be actuated by air pressure.It would also be possible to employ pressurized disengagement actuationsimply by shaping the sabot means, subcaliber projectile, and anyconnecting means, in such a manner that their alignment when engagedprior to launch acceleration will shift under the pressure of launchacceleration to a new alignment in which the positive connection isdisengaged. Such an arrangement might necessitate an additional sourceof drag or impulse, such as an indentation, protrusion, or offset in thebore, or a detent means, preferably near the breech Again, suchembodiments might be used with or without detent means, depending on ifa delay effect were needed to enhance the disengagement actuationfunction. It should be noted that the means for positive connection maysometimes be a distinct structure from the sabot and subcaliberprojectile, but in other cases may be an integral part or parts of oneor both of the sabot means and the subcaliber projectile.

Other ways to actuate disengaging of a positive connecting means includeusing a component that is engaged by the barrel, breech, or mouthpiecein such a manner as to be pulled loose from the sabot projectileassembly and retained near the breech as the rest of the sabotprojectile assembly is accelerated down the barrel bore. Also, the sabotor positive connecting means might be provided with a set of aerodynamicsurfaces that exploit lift or atmospheric drag upon exit from the barrelbore to move somewhat independently of the body of the sabot proper, orto separate a sectional sabot body, and thus to pull the positiveconnecting means loose from its engagement or engagements. Inparticular, if the additional aerodynamic surface or surfaces exits thebarrel prior to the sabot proper, and thus encounters atmospheric dragor lift prior to the sabot proper encountering atmospheric drag as thesabot projectile assembly exits the barrel bore, then the disengagingmay take place while the sabot and main portion of the subcaliberprojectile assembly are still being positively accelerated by launchthrust, greatly enhancing the disengaging function/action and allowingit to exploit higher levels of force or energy.

*It should also be noted that in some embodiments of my invention, itmay not be necessary for the subcaliber projectile and sabot means to bein direct contact or connection with each other during all phases of theloading and launching sequence. In some embodiments, the subcaliberprojectile and sabot means may be loaded sequentially rather thansimultaneously, and additionally or alternatively, rather than beingdirectly abutting while in loaded position within the bore prior tolaunch acceleration, the subcaliber projectile and sabot means maysimply be secured within reasonable proximity of one another.

Additional notes on advantages, alternative embodiments, and methods ofuse, concerned particularly with improved targets and target shootingmethods

Certain embodiments of my invention may provide a type of target andassociated method of target shooting highly suitable for use with theassociated subcaliber projectiles. Furthermore, the target and method ofshooting makes it possible for the user to substantially reduce thepotential for damage to projectiles caused by impact with the target aswell as by impact with other projectiles already lodged in the target orwith projectiles subsequently launched at the target. Also greatlyreduced is the time and effort, as well as the potential for damage toprojectiles, associated with the process of retrieving the projectilesfrom the target. This represents a very important set of advantages ofmy invention and is highly in keeping with tradition, convenience,economy, and safety in light of the fact that blowgun projectiles, muchlike the arrows used in archery, are typically and traditionallyintended to be reusable. Accordingly, after a round of shooting at atarget, the user will typically retrieve the projectiles from the targetwhere they have lodged, and begin the shooting process anew in which thedarts that were retrieved are reused and shot again at the target.

Using the target provided by my invention greatly reduces the potentialfor damage to projectiles that is associated with prior-art practices ofshooting projectiles at targets and retrieving projectiles from thetargets, and furthermore reduces the amount of time and effort spent inretrieving projectiles from the target after a round of shooting. Otheradvantages of the target and method provided by my invention is that itmakes possible a substantial improvement in the accuracy of assessmentof shot placement on the target face, and makes possible a greatervariety of target practice shooting styles and formats. Typically,targets according to prior-art usage operate in a manner comparable tocertain targets used for archery. The target face is printed upon, oralternatively attached directly to, a backing that provides sufficientresistance during penetration to catch and hold the projectile. Such atarget stops and holds the projectile, which remains lodged in, andusually protruding from, the target face until retrieved by the user.There are several ways in which this method of target shooting exposesthe projectile to potential damage. The first is that the projectilelodged in the target face is susceptible to impact by other projectilessubsequently launched at the target, which may cause damage to one orboth projectiles involved in the impact. This type of problem withimpact between projectiles may also be encountered in archery targetshooting. However, with blowgun projectiles, the full-caliber pistonportion typically presents an even larger transverse area susceptible tohits than does the aft section of an arrow shaft with attached vanes orfeathers. Furthermore, since blowguns are often used at shorter rangesthan are bows and arrows, as the user's skill increases and tightergrouping is achieved, the rate of impact incidence may rise. Theprojectile components may be pierced, punctured, broken, or bent by suchimpacts, and even if still launchable, will normally no longer beaccurate.

Another potential for damage occurs as the target catches, decelerates,and stops the projectile. If the target stops the projectile toosuddenly, the mass of the full-caliber piston portion (which istypically positioned at the rear of the projectile), even if quitelightweight, may still have sufficient momentum, and especially lateralmoment, to increase the flexing of the shaft beyond its elastic limit,resulting in permanent bending or kinking, or even breakage. Also, ifthe projectile is stopped too suddenly, the stabilizer may tear loosefrom or slide loose from its attachment to the rod, and move forwardalong the narrow rod, possibly damaging the stabilizer and forcing theuser to take the time to slide the stabilizer back into position andattempt to reattach it in place Furthermore, the end of the rod, even ifblunt, is still usually quite narrow; therefore if the stabilizer slidesforward upon the rod a portion of the stabilizer may be punctured by thenarrow rear end of the rod, and the grip of the stabilizer may bepermanently loosened, so that it is no longer securely attached to therod.

On the other hand, if the target does not stop the projectile quicklyenough, penetration will be too deep and the typically rearwardlypositioned piston portion will impact the target face. This may causemore damage to the target face, shortening target life. Moreimportantly, the impact will often also damage the piston or else stripit loose backwards from the rod, so that the user has to find andretrieve the stabilizer and reattach it to the rod. Another potentialfor damage to the projectile occurs during the process of retrieving theprojectiles from the target face. As mentioned before, the target muststop the projectile fast enough but not too fast. This, along with thefact that the rod is often very narrow and affords little surface areato be gripped by the target face, means that if the target hassuccessfully caught and stopped the projectile, then the rod will belodged very tightly into the target. The user, upon attempting todislodge or pull the projectile from the target, must firmly grasp therod, which however, in being very narrow affords little purchase for theuser's grip. The user normally cannot grasp the piston to pull out theprojectile, since this could either damage the piston or else strip itloose from the rod. The user must therefore either pinch the rod verytightly with his fingers and thumb, or else use a tool, such as pliers,to grip the rod and pull the projectile loose from the target. In eithercase, a rocking motion must often be employed to carefully work theembedded projectile loose, and care must be taken not to bend or breakthe rod during this procedure. This may cause discomfort to the user ifusing fingers, and in any case may cause lost time, extra exertion, andpossibly fatigue, during the retrieval process. Even if reasonable careis taken, it is still easy to damage projectiles during such a retrievalprocess.

There is another disadvantage encountered with target shooting withprior-art full caliber projectiles, which is also associated with thetendency of projectiles lodged in targets to be impacted by subsequentprojectiles. This tendency often makes it difficult to accurately assessand measure shot placement precisely. Even though hitting a projectilealready lodged in the target may indicate tight grouping, and may forthis reason be pleasurable to the user, it does not offer to the user,if so desired, the alternative to precisely map the point of impact ofthe projectile with the target face that would have occurred were it notfor the interference of the intervening projectile.

The problems outlined above with prior-art targets and prior-artprojectiles, may often be exacerbated when prior-art blowguns launchingprior-art projectiles at higher velocities are used.

My invention offers several ways to eliminate or minimize the potentialfor damage to projectiles associated with target shooting.

First, by using subcaliber projectiles to shoot at a conventional targetin which the projectiles lodge in the target face, the shaft and anyadditional stabilizing members present a smaller total area exposed topotential impact by subsequent projectiles, so that even with tightgrouping the rate of impact incidence will be diminished substantially.Furthermore, the smaller lateral dimensions and lighter weight of thestabilizers used in subcaliber projectiles minimizes the bending forcesthat the stabilizer mass applies to the shaft during impactdeceleration.

Second, the projectiles and the target itself may be adapted orconfigured in such a way as to completely eliminate the potential fordamaging projectile-on-projectile impact. In such a target, the targetface may be supported, or suspended, apart from and in front of animpact mat, preferably at a distance from the impact mat which issomewhat longer than the length of the projectile to be used. Theprojectiles launched at this type of target advantageously have a tipwhich is essentially blunt rather than sharp. The projectile completelypenetrates the target face and travels on to impact the impact mat. Thedistance between the impact mat and the target face is preferablysomewhat greater than the length of the projectile, in order that theprojectile may have adequate clearance for complete penetration of thetarget face before impacting the impact mat. The impact mat ispreferably adapted to yield under the projectile's impact and dispersethe impact energy without being penetrated, and without causing theprojectile to rebound back towards or through the target face. The spentprojectile then drops to a collection area below. Impact mats might, forinstance, be constructed of one or more layers of flexible, woven cloththat is preferably tightly woven, and strong enough and thick enough toresist penetration or tearing by the impact of the blunt projectiles,and preferably with sufficient weight to help to absorb the momentum andenergy of the projectile. The mat might be suspended from its top edge,with the bottom edge hanging loosely and unattached. The impact matmight advantageously be provided with one or more pockets that allowinsertion of removeable and replaceable pieces of impact resistantmaterial to reinforce areas of the impact mat that are likely to be hitmost often by projectiles. The target face might be paper, cardboard,paper mounted on cardboard, and the like. Thus such a target essentiallycomprises a target face, preferably completely penetrable by theprojectile, suspended apart from and in front of an impact mat/backstop,preferably impenetrable by the projectile, with the target face andimpact mat/backstop preferably separated by a distance somewhat greaterthan the length of the projectile. It will be apparent to one skilled inthe art how to provide a suitable housing or frame structure in which tosupport or suspend the target face and impact mat/backstop. A redundantbackstop structure may be advantageously suspended behind the impactmat/backstop in readiness for the event of a projectile unexpectedlypenetrating the impact mat/backstop, such as due to structural ormaterial failure of the impact mat/backstop.

Such an impact mat target may also be used with advantageouslyblunt-tipped full caliber projectiles, provided that the target face andany direct support of the target face may preferably be puncturedcompletely without catching on or damaging the enlarged stabilizerportion of the full caliber projectile. However, the use of subcaliberprojectiles, particularly very streamlined subcaliber projectiles,minimizes damage to the target face, extending target life, and makingpossible very precise assessment of shot placement. In particular, theblunted tip and foreshaft may be shaped in a manner so that thepenetration produces a very clean, small hole in the target face, byessentially shaping the foreshaft or head with a section forwardlyextending from the widest portion of the foreshaft and tapering to ablunt forward tip or end of somewhat smaller diameter than the widestportion of the foreshaft. Alternatively, the foreshaft or head may beshaped in such a manner to produce larger holes in the target face thatare more visible at a distance, by essentially shaping the foreshaftwith the widest portion, or a flared widest portion, substantially atthe forward end or tip of the foreshaft.

Should the user desire to use sharp-tipped projectiles on such atotal-penetration target face, but still minimize the potential forprojectile-on-projectile impacts, then the impact mat might be replacedby a backstop adapted to be partially penetrated by projectiles in orderto stop, catch, and hold the projectiles, but with the backstop furtherso adapted as to be moveable in relationship to the target face. Anexample would be a cylinder, drum, or disk, made of or surfaced with amaterial adapted to catch and hold the projectiles, and possibly shapedto form distinct facets. Such a cylinder, disk, or the like could beslowly turned or incrementally turned on an axis by motive means such asa motor, a spring, or by each succeeding impact force, or even a stringor cable pulled on manually by the user, so that projectiles lodged inthe backstop would be moved away from the area where subsequentprojectiles were most likely or more likely to strike. Incrementalturning of such a backstop could possibly be triggered or actuated byeach succeeding impact force, possibly with a ratchet or escapement typeof mechanism. Alternatively, such a revolving or rotating cylinder ordisk, rather than being used merely as a backstop, could instead be usedwithout a total-penetration target face, possibly with a separate targetface attached directly to each of any facets or subdivisions of thecylinder or disk or other backstop.

My invention also offers another strategy for increasing ease ofretrieval of projectiles lodged in a target, which may be applied toeither full caliber or subcaliber projectiles. In this strategy, theprojectile is purposefully so adapted that upon impact with a target, aportion of the projectile's energy is diverted or dispersed throughinteraction between components of the projectile, particularly when somerearward portion or member is allowed to move forward relative the restof the projectile during impact, since for every action there must be anequal and opposite reaction. Such a dispersal of energy reduces theprojectile's penetration of the target, so that the projectile isgripped less tightly by the target, and is easier to pull out. However,it does not require reduction in projectile velocity or energy inflight, nor does it require increased lateral area or other significantchanges in form factor, therefore trajectory performance issubstantially unaffected. This greatly reduces the time and effortneeded to retrieve the projectile, and reduces wear and tear on thetarget as well. An example would be a projectile in which a component ispurposefully adapted to frictionally engage the shaft in such a manneras to be able to slide forward along the shaft upon impact. Such acomponent might include the stabilizer portion of a full caliber orsubcaliber projectile, or might be structurally distinct from thestabilizer portion, such as a tubular member adapted to somewhat snuglyand slidingly fit around the projectile shaft. Alternatively, acomponent might slideably engage the foreshaft in a similar manner.After retrieval, the sliding or otherwise moveable component may bemanually repositioned nearer the back of the projectile (or otheroriginal position) prior to launching the projectile at the targetagain. Another possibility is a shock-absorbing spring means that allowsa rearward portion of the projectile to move forwards relative theforward portion and automatically restores the original position afterimpact, or in which the spring itself becomes the energy dispersalcomponent. Another example is a piston inside a hollow shaft thatslidingly engages the inner surface of the shaft, or possibly compressesor displaces air within the shaft upon impact, perhaps through a holenear the front of the shaft or a hole through the piston itself. Suchenergy-dispersing components are advantageously adapted to remain infixed relationship relative each other and relative the other portionsof the projectile during launch and during trajectory flight up untilthe moment of impact, in order to promote consistent projectileperformance. It will be apparent to one skilled in the art that thisstrategy could also be adapted for application to other types ofprojectiles, such as full caliber blowgun projectiles, or such asarchery arrows. Additional notes on advantages, alternative embodimentsand methods of use, concerned particularly with improved blowgunperformance in launching spherical projectiles and other substantiallynon-elongate projectiles

Certain embodiments of my invention may provide much needed improvementin blowgun performance in launching spherical projectiles, such asvarious sizes and types of pellets and paintballs. Such embodimentscould also be adapted to launch substantially non-elongate projectilesother than spherical projectiles. In order to appreciate thesignificance of this set of advantages it will be necessary to hereinclude some additional review of prior art.

In firearms and artillery, full caliber spherical projectiles generallyexhibit low sectional densities in comparison to full calibercylindroconical projectiles or other elongate full caliber projectiles.In blowguns, however, since full-caliber elongate projectiles are notusually solid metal, but rather typically have an affixed full caliberpiston composed of some lightweight material, it may often be thefull-caliber spherical projectiles, such as paintballs or metal spheres,which have the greater sectional densities. In fact, such full caliberspherical projectiles may often be of a sectional density too high to becomfortably or efficiently propelled by the user's breath. If, on theother hand, a full-caliber sphere composed of a lighter material such asplastic, glass, or wood is used, the decreased sectional density willoften adversely affect trajectory and accuracy. This is especially truesince it is generally more difficult to apply aerodynamic correctionalguidance to spherical projectiles, than it is to elongate projectiles.

Furthermore, typical methods of using barrel bore rifling to engage andimpart stabilizing spin to spherical projectiles used in firearms wouldcause excessive launch resistance in a blowgun. Another challengepresented by spherical projectiles is that as caliber increases, volume,and therefore mass, increases at a faster rate than does the maximumcross-sectional area. Therefore, with spherical projectiles,thrust-to-mass ratio declines as caliber increases. This helps toexplain why blowgun paintball pellets are more common in smallercalibers such as 40 or 50 caliber, rather than the larger 68 caliberpaintballs often used in CO2 powered mechanical paintball guns. However,the lighter mass and lower sectional density of the smaller paintballs,although easier to accelerate to satisfactory velocities, also resultsin low muzzle energy and rapid loss of energy to drag, which may havenegative impact on paintballs performing adequately in terms ofrupturing sufficiently on impact with a target.

Another limitation with reducing caliber to obtain performance gainswith spherical projectiles is that when caliber becomes unduly small,the flow of air from the user's lungs is excessively restricted by thesmall outlet, yielding poor or very poor acceleration and velocity, andpossibly causing discomfort to the user. Thus, it is impractical formany users to use blowguns to launch small caliber sphericalprojectiles, such as the type of steel BB pellets used in mechanicalairguns, as full caliber projectiles. However, my invention makes itpossible to use a blowgun to efficiently launch BBs and other pellets,including paintballs, by launching them as subcaliber projectiles inorder to obtain a higher thrust-to-mass ratio. Furthermore, certainembodiments of my invention may make it possible to use barrel riflingto impart spin to spherical and non-elongate projectiles, as well as toelongate projectiles, yet in such a way as to avoid excessive launchresistance. The rifling employed might either be recessed grooves in thebore, or else extensions or protrusions from the bore, or a combinationof both, with the sabot provided with its own extensions or grooves ornotches, as appropriate, sized, shaped, positioned, and oriented tocooperatingly engage the bore rifling. In this way, by using apre-formed sabot that is already of the shape necessary to securely andsmoothly engage the rifling, it is not necessary for the thrust of theuser's breath to do the extra work of forcing the sabot onto the riflingwith sufficient force to grave the sabot, which would likely causeexcessive launch resistance and result either in low velocities or elsein failure of the projectile to exit the bore. Use of such sabots wouldalso make it possible to use barrel rifling to stabilize paintballs withspin transmitted through the intermediary sabot, rather than engagingthe paintball directly with the rifling, which would prematurely rupturethe frangible paintball. Additives such as ferrous particles, oralternatively, flexible magnetic tape or film, could provide ways tomanufacture paintballs that are susceptible to magnetic attraction.Since it is within the ability of those skilled in the art to createparts of molded plastic and the like which are susceptible to magneticattraction, it would also be possible to make paintballs in which any orall of the gelatin capsules, paint filling, or additional flexiblestructures incorporated therein are attractable by a magnet.

Suction is another method of securing sabots and pellets, such aspaintballs, as well as other types of projectiles besides pellets,together in launch position. A mechanical detent disengaged by launchpressure could also be used to secure a saboted paintball in loadedposition within the bore. Alternatively, a sabot might be shaped tosufficiently encapsulate a paintball or other subcaliber projectile soas to prevent the paintball from premature forward displacement relativethe sabot, yet with hinged, flexible, or separating sections allowingthe sabot to open up once clear of the bore and allow separation tooccur.

Additional noted on certain advantages, alternative embodiments andmethods of use, concerned particularly with improved internal ballisticcorrectional guidance applied to the projectile, resulting in improvedstability and accuracy of the projectile:

Prior art blowguns typically provide substantial correctional guidanceduring launch acceleration to the typically aft-ward, full caliberpiston portion of elongate projectiles by the guidance provided by thebarrel or launch tube, which normally has a straight bore transverselysized and shaped so that the full caliber piston portion substantiallytransversely fills the bore. This arrangement does not absolutelypreclude lateral deviations of the aft end or piston portion due to thetypically requisite slight looseness of fit of the piston within thebore, but does typically limit such lateral deviations to small or verysmall distances. However, the forward end of the projectile, which isnormally the forward tip of a slender rod, is usually the only point ofcontact between the bore and the rod, since the rod typically anglesdown from its point of attachment with or insertion into the center ofthe piston portion to rest upon the bore. This point of contact at theforward tip of the rod provides only a very small area of supportcontact with the bore, and thus very minimal direct guidance is appliedto the forward end of the projectile by the bore during launchacceleration. This small, essentially non-elongate area of contact isusually the rod's only point of direct contact with the bore. Thisarrangement, in conjunction with the often slightly loose fit of thepiston within the bore, typically necessary to avoid excessive friction,may leave some substantial play in the orientation of the projectile.Particularly, the forward tip of the rod may slide upon the bore andswing towards the left or right, or possibly even oscillate back andforth from side to side. The tip of the rod may also lift off the bore,due to play of the piston or to barrel curvature, such as that caused bygravity-induced sag, in which case no guidance is applied to the forwardend of the rod unless contact with the bore is reestablished essentiallyby luck or happenstance. Thus the projectile may exit the bore andcommence external flight without being initially aligned substantiallyparallel with the longitudinal bore axis or with the initial directionof travel.

The stabilizer portion of either a full caliber or subcaliber projectilemay in many instances or situations be able to fairly quickly re-align aprojectile with or parallel to the direction of travel, if theprojectile does happen to exit the bore oriented at somewhat of an angleto the initial direction of travel. However, it may nevertheless bepossible for the guidance efficiency of the stabilizer portion(particularly if the projectile does not have a particularly stableoverall balance) to be temporarily compromised by either the initiallyslanted orientation of the projectile, or possibly as well byperturbations transmitted to the dart during launch. Such perturbations,which might be characterized as yaw, pitch, sideslip, or morecomplicated types of motion, we will refer to for simplicity's sake asrotational motion. Such slanted orientations or rotational motion orboth may change the air flow behavior over the aerodynamic controlsurfaces of the projectile, thereby temporarily lowering theirefficiency and slowing response time to correct deviations. Although themaximum possible total lateral displacement of the projectile's forwardend during launch would seem to be relatively small, bounded by thetransverse dimensions of the bore, the fact that any such displacementtakes place during some portion of the very short length of time that ittakes for the projectile to travel through and exit from the bore meansthat the projectile may acquire a rotational velocity or rotationalmoment which, although it may at first glance seem rather low, isnevertheless substantial enough to lower or compromise stabilizerefficiency. In extreme cases, tumbling end over end may result, however,even in mild cases when stability and orientation are quickly recovered,and the rotational motion is canceled or damped out, a deviation willalready have been introduced into the trajectory at substantially thebeginning of the trajectory, which means that the deviation may beamplified during substantially the entire external flight of theprojectile.

Perhaps even more importantly, the deviations described above take placein an essentially inconsistent, non-repeatable, unpredictable fashion,since each projectile may exit the barrel bore with a differentorientation and different rotational motion from the previous dart.However, accuracy in shooting generally demands as much consistency andrepeatability from shot to shot as possible. Even substantialdeviations, if they are reasonably consistent and repeatable from shotto shot, will result in tight grouping and thus may be compensated forduring aiming to yield good on-target accuracy. On the other hand,inconsistent, non-repeatable deviations will remain unpredictable anddefy compensation efforts.

My invention makes it possible to improve internal ballistic guidanceand stability of the projectile in at least two possible methods. Thefirst method relies on the fact that in certain embodiments whichutilize a magnetic projectile detent, and in which the projectileincludes a flexible shaft and a magnetically attractable foreshaft (orin certain embodiments some other magnetically attractable portion), theattraction of the magnetic detent pulls substantially the entire lengthof the foreshaft, along with any overlapping portion of the shaft, downupon or parallel to the inner surface of the bore, and parallel to thebore axis as well, thereby creating an elongate area of surface contactbetween the projectile and the bore. However, the consequent flexing ofthe shaft, as well as any possible play in the orientation of the sabotwithin the bore, allows the shaft to remain securely engaged by thesabot means. Alternatively, with either a flexible shaft or a rigidshaft, the sabot may be adapted to engage the shaft at a portion of thesabot that is nearer to or even adjacent to the bore surface, ratherthan at the center or axis of the sabot. The freedom to use assymetricalsabots without detriment to the aerodynamic properties of the projectileproper makes such an off-center engagement even more viable. Anotherpossibility for achieving a similar projectile orientation is using arigid shaft attached by a hinge or flexible intermediary member to arigid foreshaft. It would also be possible in certain embodiments toachieve similar effects when using a mechanical projectile detent orother non-magnetic projectile detent, along with a projectile whichmight not contain a magnetically attractable portion.

When the foreshaft is pulled by the detent down upon or essentiallyparallel to the bore's surface, the elongate portion of the subcaliberprojectile in contact with the bore's surface occupies an area ofsurface contact with the bore that is rather like a substantiallyelongate line segment or a slender rectangle, in contrast with thealmost point-like, small, substantially non-elongate area of contactbetween the projectile's forward end and the bore's surface that istypical with many prior-art full caliber projectiles. Such an increased,longitudinally elongated area of surface contact (which mayadvantageously be substantially aligned parallel to the longitudinalaxis of the bore) does not significantly increase launch resistance, butI believe that it does provide significantly increased resistance toside-to-side sliding or transverse displacement of the projectile orprojectile forward end. I believe that in certain embodiments thiseffect may be amplified by the formation of a mild suction or mildadhesion between the foreshaft and any overlapping portion of the shaftin contact with the inner surface of the bore, as a result of theattractive pull between the detent and the foreshaft or other portion ofthe projectile susceptible to magnetic attraction. Furthermore, Ibelieve that in certain embodiments the tension of the flexed shaft,along with the acceleration of the sabot against the inertial mass ofthe projectile, creates an oppositionally directed tension. I believethat such an oppositional tension tends to help the sabot and theforward portion of the projectile to keep each other slidingly anchoredon the surface of the bore, consistently positioned upon a certain sideof the bore, or in a certain substantially consistent position relativethe cross-sectional shape of the bore, so as to follow a substantiallystraight line path along and through the bore, rather than bouncingaround from side to side or top to bottom within the bore, during launchacceleration. I believe that in this manner, inertia counteringacceleration, along with the flexing of the shaft, keeps the foreshaftslidingly anchored upon the bore surface even after the sabot projectileassembly breaks free of the detent's influence. Even if any suchbouncing of the sabot should occur during launch travel, the flexibilityof the shaft in certain embodiments may help to resist transfer of thebouncing motion to the foreshaft. Thus, it may be seen that certainembodiments which include a magnetic detent, and in which the projectileincludes a flexible shaft and a magnetically attractable foreshaft (orin certain embodiments some other magnetically attractable portion), mayprovide greatly improved internal ballistic stability. It will beapparent to one skilled in the art that a similar effect may be achievedin certain alternative embodiments which use other types of detents,such as a mechanical detent, to pull an elongate portion of theprojectile substantially flat against the surface of the bore while inloaded position. It will also be apparent that a similar effect can beachieved with a projectile that either does or does not have a flexibleshaft or other flexible portion, by adapting the projectile and sabot toengage each other in such a way that the entire length of theprojectile, or some substantially elongate portion of the length of theprojectile, may lie flat upon the inner surface of the barrel bore,which in certain embodiments may require the projectile to engage thesabot asymmetrically rather than at the central region of the sabot'sforward end.

My invention also provides another method by which improved internalballistic stability may be achieved, and which may be used withprojectiles with either flexible or rigid shafts. In this method, thebarrel bore is provided with one or more substantially straight,longitudinally aligned guidance grooves or projections in or on thebore's inner surface, and which extend along substantially the fulllength of the bore and are substantially parallel to the axis of thebore. In general, each such groove or projection should extend all theway to the muzzle and be transversely open at the muzzle end. The grooveor projection should preferably extend close enough to the breech endthat, when the sabot projectile assembly is loaded within the bore, thetip or length of the foreshaft, or other cooperating portion of theprojectile as appropriate, may rest in or against the groove orprojection. If the guidance groove or projection does extend all the wayto the breech end, it may be either open or closed at the breech end.Any such guidance grooves preferably should be of sufficient depth toprovide adequate guidance to the cooperating portion of the projectile,and should be of sufficient width to allow the cooperating portion ofthe projectile to slide along the groove without any binding orexcessive friction, yet any such groove should also be narrow enough toprovide a precise degree of guidance to the cooperating portion of theprojectile. Guidance grooves of various cross-sectional shapes might beemployed, including grooves within grooves, or projections withingrooves. Alternatively, the projectile may be provided with one or moreextensions or protrusions, affixed to or integral with the forwardportion or other suitable portion of the projectile, with any suchprojectile extensions adapted to engage cooperating guidance grooves orprojections in the barrel bore. The sabot might also be provided withone or more extensions for cooperatingly engaging guidance grooves orprojections of the bore. If the bore is provided with one or morelongitudinal guidance projections, the projectile or the sabot or bothmay be provided with notches or grooves adapted to be cooperatinglyengaged by the bore projections or to provide transverse clearance forthe projections. Alternatively, the sabot may be adapted to be somewhatflexible or compressible, or may be sized somewhat smaller to fit thebore more loosely, in order to provide transverse clearance for any suchguidance projections. A projection might also itself be grooved. Anexample would be a single longitudinally grooved longitudinalprojection, which could be considered to be equivalent to two parallellongitudinal guidance projections, and which would essentially provide atrack or channel for guiding some cooperating portion of the projectile,and which might possibly be used with a sabot means which is grooved,notched, or even of an essentially u-shaped or inverted-u-shapedcross-sectional shape, so as to provide transverse clearance for theguidance projection or projections. Longitudinally elongated projectionsor indentations of the bore might in certain embodiments also provide ameans to further limit transverse bounce or play of the sabot, with onlya slight increase in snugness of fit or friction with the barrel bore.In fact, use of such longitudinal projections, if deployed or configuredcorrectly, could actually reduce bearing surface contact between thesabot and the bore, and thus reduce friction and launching resistancewhile increasing the precision of guidance of the sabot or stabilizer.It may be appreciated that the use of grooves or projections or acombination of both, as outlined above, could also be applied tolaunching full caliber projectiles with increased internal ballisticstability or reduced bearing surface contact, or both. Because thebarrel with longitudinal bore grooves or protrusions provides enhancedinternal ballistic performance and possibly reduced bearing surfacewhether used with full caliber projectiles or sabot projectiles, it isdesired that protection be provided to this area whether used inconjunction with other features of my invention or used as a stand-alonesolution, as is true also for the use of other features of my inventioneither conjointly, or individually in stand-alone applications.

Any such guidance grooves or projections in the barrel bore shouldadvantageously be of sufficient transverse dimensions to providesufficient surface engagement of the projectile and/or sabot to ensureadequate guidance, yet preferably with transverse dimensions smallenough to limit any air seal losses as much as possible. Sabots mightoptionally be provided with extensions to substantially cooperatinglyfill any transverse gaps within grooves or around or betweenprojections, thereby keeping any air seal losses to a minimum. Guidancegrooves or extensions might be transversely directed or aligned radiallytowards the axis of a bore with a circular disk-shaped cross-sectionalshape, however such grooves or extensions would not have to betransversely aligned radially, and such grooves or extensions could alsobe used in bores with alternate (non-circular disk-shaped)cross-sectional shapes. For example, the grooves or extensions might betrans-versely aligned in a rectilinear horizontal and vertical fashionrather than in a radially aligned fashion, with transverse dimensions ofextensions or grooves so adapted to provide a good cooperating fit forthe projectile assembly. It may be appreciated that extensions of thebore surface, or of the projectile, would make it possible to usealternate bore cross-sectional shapes with little or no increase in theamount of bearing surface contact area and friction between the sabotand the bore. This is important because a circle encloses a given amountof area with the minimum perimeter possible. Thus using a differentcross-sectional shape for the bore (other than a circular disk) wouldotherwise normally result in an increase in bearing surface andfriction. Applying internal ballistic aerodynamic effects to the sabotprojectile assembly during launch, such as aerodynamic lift, groundeffect lift, and spoilers might also be more easily employed with boresof alternate cross-sectional shapes. Fairly rigid skeletal structureswhich support thin film membranes to provide sabots or pistons might insome embodiments be more easily adapted to fit bore cross-sectionalshapes that have substantially straight sides rather than circularlycurved sides.

Any longitudinal guidance groove or projection in the bore, along withcooperating portions of the projectile or sabot or both, may alsopossibly be further adapted so as to resist any tendency of thecooperating portion of the projectile to lift up and away from securecontact with the guidance groove or projection. An example would be alongitudinal guidance groove with a longitudinal overhanging lip at thetop edge of one or both sides of the groove, so that the transverse gapbetween the overhanging lips/edges is somewhat narrower than thetransverse width of some portion of the groove beneath the overhanginglips. Such a modified guidance groove might be used in conjunction witha projectile in which, for example, a portion of the forward end issized to slide easily through the widest transverse portion of thegroove, yet is too wide, after being inserted into the breech endopening of the guidance groove, to lift vertically through the narrowergap defined between the overhanging lips of the groove. If necessary,the projectile might also be provided with a portion narrow enough topass through the gap between the groove lips and connect with a fixedpiston or a sabot. Alternatively, the entire length of the projectilemight rest within the groove beneath the overhanging lips, and a sabotbe provided with an extension narrow enough to pass through the gapbetween the groove lips and rearwardly engage some portion of theprojectile.

In certain embodiments, the depth or height of a guidance groove orprotrusion might be selectively varied along its length in such a way asto offset any tendency of the barrel and bore to sag under the pull ofgravity. It will be apparent to one skilled in the art how to vary thedepth or height of a guidance groove or protrusion in such a manner thatwhen the barrel or bore sags under the pull of gravity, the guidancegroove or protrusion compensates for any sag to define a substantiallystraight line path along the appropriate dimension.

Overview and Summary of Some Advantages

My invention makes it possible to use sabots with subcaliberprojectiles, which, in comparison to a reference full caliberprojectile, therefore:

1. Makes possible higher sectional density, and2. Very streamlined form factor, thereby yielding3. Increased ballistic coefficient;4. and also, within practical limits, makes possible higherthrust-to-mass ratios, by either:5. Decreasing the subcaliber projectile mass, or6. Increasing the caliber bore, or

7. Both.

It may be noted that any of the three possibilities described in numbers5, 6, or 7, directly preceding, may be done in such a manner as toprovide a subcaliber projectile which still has higher sectional densitythan a reference full caliber projectile, after discarding of the sabotoccurs, as long as the subcaliber projectile's mass is not excessivelyreduced in comparison to the controlled mass of the reference fullcaliber projectile.

Certain embodiments of the blowgun and sabot projectiles provided by myinvention may exhibit highly desirable performance characteristics whencompared to reference full caliber blowgun projectiles, such as any orall of the following: Subcaliber projectile characteristics such ashigher thrust-to-mass ratio, higher sectional density, more streamlinedform factor, higher ballistic coefficient, and reduced drag maytranslate into one or more performance advantages such as, for example,increased exit velocity, flatter external trajectory, and more energyand velocity retained down range. Flatter trajectories in turn translatedirectly into increased accuracy, since the consequent reduction invertical drop of the projectile, particularly at extended ranges, makesit easier for the user, when aiming, to compensate for the relativelysmall or decreased vertical drop, particularly at extended ranges.Increased velocity and/or reduced drag also yield extended maximum rangeand extended effective range. It is also believed that theforward-of-center balance and radial or lateral compactness of certainembodiments of the subcaliber projectile make such embodiments morestable and accurate in-flight than a typical full caliber fixed pistonprojectile, and less susceptible to deflection in-flight by wind.Furthermore, higher launch velocities and/or extended retention ofvelocity ensures stronger airflow over any aerodynamic control surfacesof the projectile throughout a greater portion of the trajectory whencompared to a projectile with lower launch velocity and rapid decreaseof velocity. Furthermore, accuracy may be improved by the consistency ofpositioning and orientation or alignment of the subcaliber projectileduring each shot by the detent. I believe that the detent systempositioning of the subcaliber projectile provides another unexpectedbenefit of my invention in terms of improvement in internal ballisticstability during launch acceleration, which translates into improvedaccuracy and stability of the projectile on its external trajectory. Inaddition to the consistent positioning and orientation, the temporaryflexing of the flexible shaft in certain embodiments allows the detent'sattraction to pull substantially the entire length of some elongateportion of the foreshaft, along with any overlapping portion of theshaft, substantially flat against the inner surface of the barrel bore,and thus aligned substantially parallel to the longitudinal axis of thebore, and consequently as well to the initial direction of travel alongthe projectile's external trajectory. I also believe that during lunchacceleration the push of the sabot and the inertia of the foreshaftkeeps the shaft flexed and the forward portion of the projectile pressedagainst the bore's inner surface during the entire travel of theprojectile through the bore during launch. This type of orientation andsurface contact of an elongate portion of the projectile against theinner surface of the bore may result in an increased resistance tosideways movement of the forward end of the projectile during travelalong the bore by applying a much greater degree of guidance to theforward end of the projectile during lunch acceleration, when comparedto the minimal degree of guidance typically applied to the forward endof a typical prior art fixed piston full caliber projectile, in which(considering the forward end of the projectile only) only the tip of theforward end of a relatively rigid rod-like section of the projectile isin direct contact with the bore.

I believe that a similar effect may be achieved by adapting the sabotmeans to engage the subcaliber projectile in such a manner thatsubstantially the entire length, or an extended portion of the length,of the subcaliber projectile may be positioned flat against the boresurface, in which case the subcaliber projectile's shaft could be eitherflexible or relatively rigid. Another way of enhancing the internalballistic correctional guidance in some embodiments of my invention isto provide one or more substantially straight longitudinal grooves inthe bore's inner surface, with the groove or grooves substantiallyparallel to the longitudinal axis of the bore. Such a groove would beadvantageously cross-sectionally dimensioned so as to providesubstantially precise guidance to the forward end of the subcaliberprojectile or to the widest cooperating portion of the subcaliberprojectile in contact with the groove, without binding or unduefriction. The subcaliber projectile might be positioned resting in thegroove in several ways, such as, for example, full length surfacecontact, with partial length contact of a forward section (with a flexedshaft), or with forward contact of substantially only the tip of theshaft or foreshaft, and in any of such cases, groove guidance may beapplied to any cooperating portion or portions of the projectile.

The sabot may also be adapted to engage any such longitudinal guidancegroove or grooves so that enhanced guidance is applied to control theorientation and position of the sabot as it travels down the bore. Asimilar effect may be obtained by providing the inner surface of thebore with two parallel longitudinal protrusions between which theforward portion or other cooperating portion of the subcaliberprojectile may rest, and by which the projectile may be slidinglyengaged and guided during launch travel down the bore. The sabot may,for example, be flexible, or sized slightly smaller, or notched, or somecombination of such options, in order to allow the sabot toaccommodately slip over any such longitudinal bore guidance protrusionsduring launch travel.

It will be readily apparent to one skilled in the art that theprinciples of my invention will lend themselves to application toprovide numerous alternative embodiments. The embodiments with conicalsabot and slender elongate subcaliber projectile with foreshaft andshaft described in FIGS. 1-51 above were chosen as particularly suitableillustrative examples because they function well, are versatile, and arealso well-suited for a version of my intervention in which the user mayassemble or make some or all of the components of the blowgun, sabots,and projectiles themselves. This kit approach will be explained furtherbelow.

Notes mainly on alternative embodiments of the sabot and the projectile

A conical shell sabot, such as either of the ones included in theembodiments described above in FIGS. 1-43, may be molded from plastic orplastic foam, or rolled and trmmed from plastic film or paper that hasbeen suitably treated to the water resistant. It could also be made fromother materials, such as, for example, cardboard, or papiermâché. Evenwhen a conical shell sabot is formed by rolling flexible film or paper,a conical shell, in general, especially considering its light weight,allows excellent strength in the portion near the tip, which portionnear the tip is in certain embodiments where the subcaliber projectileengages the sabot. A conical shell sabot could in certain embodiments beported at the tip by truncating the tip slightly. Such a porthole couldserve as an air pressure equalization passage to help prevent anytendency for a partial vacuum to form within the subcaliber projectileshaft due to the possibility of the sabot tip being pushed slightlydeeper into the shaft, particularly if the rear end of the shaft mighttemporarily give or expand slightly under the strong forward push of thesabot during launch acceleration. Another way to prevent the formationof such a partial vacuum or suction between the subcaliber projectileand the sabot would be to provide pressure equalization ports throughthe foreshaft or through the shaft, or to provide grooves orcorrugations in certain sabot and projectile surfaces, such as theforward surface of the sabot or in the rearward surface of thesubcaliber projectile shaft, in such a manner that when the subcaliberprojectile and the sabot are engaged, the grooves, corrugations, orports allow pressure equalization airflow between external air and anyairspace contained between and defined by the subcaliber projectile andthe sabot.

On the other hand, a lightweight solid cone sabot could be molded fromstrong lightweight foam, for instance, preferably a relatively rigidtype of plastic foam. Or conical sabots could be formed which combinesolid portions with hollow shell portions.

Whether shell or solid, a conical sabot may, in some embodiments,advantageously be provided, at its tip or other forward facing portion,with a forwardly extending elongate slender protrusion. This slenderprotrusion might be molded or machined as an integral part of the sabot,or alternatively might be a distinct structure, such as a slenderelongate plastic bristle, affixed to the sabot by means such asinsertion through a cooperating hole through the sabot and securingtherein by frictional engagement or glue. The slender protrusion ispreferably substantially much narrower than the inner diameter of thesubcaliber projectile shaft, so that when inserted inside the shaft, itencounters negligible frictional engagement with the inner surface ofthe shaft, and therefore encounters negligible resistance to slidingback out of the shaft. There are several uses for such a slender tipprotrusion. One of them is in an embodiment of my invention in which,after the subcaliber projectile has been inserted into the bore and isheld partially-loaded within the bore by the projectile detent beforethe sabot is inserted, the rear end of the projectile shaft is neitherflush with, nor protruding past and out, the breech opening of the bore,but is rather in effect withdrawn a distance within the bore from thebreech. Such a partially-loaded, withdrawn positioning of the subcaliberprojectile may be necessary when using a magnetic detent in which themagnetic field is not of sufficient strength and dimension to securelyengage the projectile foreshaft over a relatively wide range of motion.In some instances, a sabot cone without a slender tip protrusion couldbe used with such an embodiment in which the rear end of thepartially-loaded projectile's shaft is not flush with or slightlyprotruding from the breech, without too much difficulty. Particularly aslong as the rear opening of the partially-loaded shaft remains within adistance of the breech opening that is substantially less than thelength of the sabot cone, it will often still be fairly easy for theuser to insert the tip of the cone into the rear opening of the shaftwithout undue difficulty. Otherwise, however, it is often much easierfor the user to first insert the tip of such a slender protrusion asdescribed above into the rear opening of the shaft, so that the looselypenetrative engagement of the protrusion within the shaft will guide thetip of the sabot cone into the rearward shaft opening as the usercontinues to push the sabot forward. Or, if the user should choose usethe essential method depicted in FIGS. 35-37, to load the subcaliberprojectile and the sabot into the bore simultaneously rather thansequentially, a slender tip protrusion of sufficient length forwardlyaffixed to or integral with the sabot would allow the user at some pointduring the insertion process to loosen his manual hold somewhat to letthe projectile be pulled into place by the magnetic projectile detent,temporarily breaking abutting engagement with the sabot, yet with aforward portion of the slender protrusion remaining within theprojectile shaft to prevent excessive lateral dislocation of the sabotrelative the projectile, and to thereby guide the sabot tip as the usermanually pushes the sabot forward to resume secure abutting engagementwith the projectile. Another example of a possible use for a sabot coneprovided with a slender tip protrusion would be in an embodiment andmethod of use similar to the one depicted in FIGS. 1-21, in which such atip protrusion would allow the user to tilt the barrel at somewhat lowerangles of elevation without causing gravity-induced lateral dislocationof the sabot relative the projectile.

It may be noted that the embodiments of sabot cone and subcaliberprojectile depicted in FIGS. 1-43, when engaged together to form thesabot projectile assembly, assume a loosely penetrative or looselynesting relationship in which the sabot cone plays a male role, and thesubcaliber projectile plays a female role. Alternative embodiments arepossible that essentially reverse any penetrative or nestingrelationship and cast the subcaliber projectile in the male role and thesabot in the female role. A simple example could be obtained by turninga conical shell sabot backwards so that after loading, the sabot cone'spointed tip is facing rearward towards the breech, and the sabot cone'shollow base is facing forward towards the muzzle, with the rear end ofthe projectile shaft abuttingly and loosely penetratively engagedagainst and within the forward-facing inner surface of the hollow shell,so that the subcaliber projectile plays a male role and the sabot playsa female role in the loosely penetrative aspect of their engagement. Itwill be apparent to one skilled in the art that alternatively, a shellor solid conical sabot, intended to be loaded with its base facingrearward toward the breech, could be truncated at the tip, and theresulting frustum could be provided in its forward end with a hollowsocket that is adapted to be loosely penetratively or loosely nestinglyengaged by the projectile's rear end when the sabot rearwardlyabuttingly engages the projectile. Such a socket in the forward end ofthe sabot allows the projectile to play a male role and the sabot toplay a female role when engaging each other. Such a socket might beadvantageously somewhat wider in diameter or dimension than the rear endof the projectile shaft, in order to prevent excessive frictionalengagement with the shaft. A socket with beveled sides that taper from arelatively wide forward opening down to a rear wall that substantiallymatches the size and shape of the shaft's rear end, may offer relativelysecure engagement against lateral dislocation of the sabot relative theprojectile, without creating excessive frictional engagement between thesabot and projectile. It should also be noted that such sabots withforward sockets could be used with projectiles that have solid shaftsrather than hollow shafts, or in which the hollow shaft has been filledwith a plug or matrix or other filler material. It should also be notedthat in certain embodiments, a projectile shaft might be either solid orsolidly filled for most of its length, but with a hollow section orhollow socket at the rear of the shaft that could be loosely penetratedby a male sabot.

It will be apparent to one skilled in the art that various forms andshapes such as, for example, cones, frustums, cylinders, spheres, disks,or various portions or combinations of such shapes or forms, or variousother shapes and forms, either in solid or shell version (or acombination of solid and shell), may readily be adapted to providesuitable sabot means, depending on the particular embodiment of theblowgun and associated sabot projectiles. Such alternative sabotembodiments could be either male sabots or female sabots, according tothe particular embodiment and method of use, and possibly also dependingon, for example, whether such alternative sabot forms were providedeither with forward end sockets, or else with slender forward front endprotrusions.

It will also be apparent to one skilled in the art that embodiments arepossible in which neither the sabot nor the projectile plays either amale or female role when engaged together. An example is embodiments inwhich there is simply an abutting engagement between sabot andprojectile with no penetrative engagement between them. An example ofsuch an embodiment was described briefly above, as an alternativeembodiment obtained by taking the essential embodiment depicted in FIGS.1-21 and replacing the conical shell sabot with a sabot comprising alightweight foam cylinder sized to substantially match the caliber ofthe barrel bore. It should be noted that if such a foam cylinder weresomewhat compressible or resiliently compressible, during loadinginsertion or launch acceleration, when the sabot was being forcefullypushed forward against the projectile, the resulting compression of thesabot could temporarily result in the projectile playing a male role andthe sabot a female role.

It will be further apparent to one skilled in the art that embodimentsare possible in which both sabot and projectile each have both male andfemale roles, or in other words in which the sabot and projectile eachhave one or more portions which penetrate the other, and in which eachhave one or more portions which are penetrated by the other. Tosummarize, then, it is apparent that embodiments are possible in whicheither a portion of the sabot is penetrated, preferably loosely, by aportion of the subcaliber projectile, or in which a portion of thesubcaliber projectile is penetrated, preferably loosely, by a portion ofthe sabot, or in which neither of the sabot and the projectilepenetrates the other, or in which both the sabot and the projectile eachhave portions which penetrate, and portions which are penetrated by, theother.

It should be noted that any nesting relationship between the sabot andprojectile does not have to be a loosely nesting relationship, as forexample in the sense of the following explanation: In certainembodiments, a socket in the sabot (or the projectile) may match to adesired precision some or all of the contours of the cooperatingpenetrating portion of the projectile (or sabot). An example would beusing a sabot provided with a beveled-sided forward facing socket, asdescribed above, in cooperation with a projectile in which some portionof the rear end has a taper that substantially matches the bevel of thesocket's side or sides so that some portion of the tapered rear end ofthe projectile nests within some portion of the beveled socket fairlyprecisely, yet without providing any substantial resistance to axialseparation of the sabot and projectile. Grooved, ported, textured, orcorrugated nesting contact surfaces might be advisable to provide airpressure equalization passages and prevent the possibility of creating asuction or partial vacuum between any substantially precisely nestingportions or surfaces of the sabot and the projectile.

It will also be apparent to one skilled in the art that certainembodiments of the sabot are possible which do not engage the rear endof the projectile. Although some portion or surface of the sabot maygenerally rearwardly abuttingly engage some rearward-facing contactportion or surface of the projectile, such a rearward-facing contactportion or surface of the projectile may either be positioned at therear end of the projectile, or alternatively may be positioned elsewherein or on the projectile.

It should be noted that the conical shell sabot and the elongatesubcaliber projectile, with proportionally short heavy foreshaft andlong lightweight shaft, such as the illustrative embodiments depicted inFIGS. 1-43, represents only one of many possible types of alternativeembodiments of sabot means and subcaliber projectile suitable for launchfrom the blowgun provided by my invention. There are several reasons forchoosing this particular embodiment for depiction as an exemplaryillustrative embodiment in FIGS. 1-43, said reasons including that theconical shell sabot and elongate subcaliber projectile with foreshaftand shaft:

1. have a good all-around versatility, and may serve as a basis for manyembodiment variations suitable for target shooting, flight shooting, andhunting applications, and2. are relatively easy and economical to assemble or make frompre-existing parts, and are relatively easy and economical to repair orreplace if damaged, and3. are suitable for embodiments which may be easily adapted as part ofan adapter accessory or converter kit for accessorizing or converting apre-existing blowgun to be able to launch sabot projectiles. Likewise,an external magnetic detent, similar to detent 210 included in theembodiment depicted in FIGS. 22-43, would be especially suitable forattaching to a barrel tube of a pre-existing blowgun without any needfor extensive modification to the barrel, and thus especially suitablefor adaptation as part of an accessory or converter kit for preparing apre-existing blowgun to launch sabot projectiles.Some notes on certain embodiments especially suitable for adaptation asdo-it-yourself projects or kits:

The following list indicates several considerations that makeembodiments similar to the embodiment depicted in FIGS. 22-43 especiallywell-suited to adaptation for do-it-yourself projects or kits, andsuggests a do-it-yourself method by which the user can make or assemblean embodiment closely resembling the embodiment depicted in FIGS. 22-43:

1. The conical sabots are relatively easy to make from a paper, aplastic film, or other flexible and reasonably lightweight and waterresistant material, which may be rolled, glued or taped, and trimmed byhand into the appropriate shapes and sizes, using either common tools(such as, for example, scissors and circle templates), or else morespecialized tools (such as, for example, paper punches) for fasterproduction rates.

2. The elongate tubular projectile shaft may be economically andconveniently supplied by various types of plastic tubing. A readilyavailable and economical source is the type of narrow, tubular, plasticbeverage straws which are popular for stirring and sipping beverages.These straws typically have a cross-sectional diameter of approximatelyone-eighth inch, being significantly narrower than the approximatelyquarter-inch diameter soda straws, and if of good quality or grade inmaterial and forming, such straws possess a combination of resilientflexibility, straightness, light weight, and appropriate length (rangingfrom about 5 to 7 inches or somewhat more or less uncut, and easily cutto other lengths with blade or scissors), to function well ascombination shafts and aerodynamic stabilizers for the subcaliberprojectiles. The straws are also generally quite cheap to replace ifthey break or split during use. Any tendency of the straws to split atthe ends under impact, or wedging of the sabot cone, may be counteractedby some type of reinforcement such as a wrapping of tight strongadhesive tape, possibly sealed against moisture with glue or epoxy. Sucha tape wrapping makes an effectual tightly fitting reinforcing band. Thenarrow, approximately eighth-inch straws are particularly well suitedfor making very streamlined elongate projectiles, however, wider tubingor straws, such as approximately quarter-inch soda straws, may also givegood or satisfactory results for certain embodiments, or may even bemore suitable for certain embodiments.

3. One do-it-yourself method by which the user may create suitable bluntprojectile foreshafts, suitable for target shooting and certain types ofhunting, is by using finishing nails with a shank diameter narrow enoughto slide inside the sipper straw shaft, while the finishing nail alsopreferably has a compact nailhead with a diameter slightly larger thanthe outer diameter of the sipper straw shaft. If the fit of the nail'sshank inside the sipper straw shaft should happen not to be snug enoughto securely frictionally engage the shank within the shaft, a gasket orbushing may be formed around the shank of the nail by various methods,such as a wrapping of tape or adhesive plastic film around the shank tosuch a thickness as will provide the desired snug fit and frictionalengagement with the straw shaft. It is also advantageous to make anothersimilar bushing between the insertion bushing and the head of thefinishing nail, which is somewhat wider than the insertion bushing, soas to form a shoulder bushing for abuttingly engaging the forward end ofthe sipper straw shaft. It is preferable that any bushing, as well asthe outer diameter of the sipper straw, should be somewhat narrower thanthe diameter or widest diameter of the blunt compact nailhead of thefinishing nail, so that the nailhead contains the widest portion of theprojectile. This promotes better aerodynamic stability, I believe, andmay also provide advantages in penetration. The pointed end of thefinishing nail is preferably snipped off with a tool such as wirecutters, bolt cutters or pliers, and the remaining truncated end of theshank smoothed with an abrasive means, in order to avoid possible damageto the straw shaft, particularly the interior of the straw shaft, duringany flexing of the shaft during loading, launch, or target impact. Theuser may also adjust the mass and balance of the projectile by furthertruncating the nail at the end opposite the end with the nailhead. Toadd mass, the user may, for example, fill part of the straw shaft with afiller such as putty, clay, plaster, cement or epoxy, possibly withbeads, sections of nail shaft, or other filler items set in the putty orepoxy or other matrix. When used with epoxy, for example, such atechnique may form, in effect, a tightly fitting plug extension of theforeshaft that may be frictionally secure within the shaft even if theepoxy or other filler does not form a secure chemical bond with theplastic of the straw. A shoulder bushing of the type described above mayhelp to cushion the forward end of the shaft and further protect it fromsplitting during launch or target impact. Another advantage to such aprojectile foreshaft made from some portion of a finishing nail, andpossibly provided with one or more insertion bushings or shoulderbushings or both, is that such a foreshaft is very durable, iseconomical to make, and, should the straw shaft break during use, suchbushings would make it especially easy to remove the broken shaft bysliding it off the foreshaft, and then easily sliding on a replacementshaft.

some Additional Notes, Descriptions, and Suggestions Regarding PossibleAlternate Embodiments:

1. The blowgun may be operated as either a breech-loader or amuzzle-loader, depending on the particular embodiment and particularmethod of use.

2. Certain embodiments may include one or more chambers or cartridgesinto each of which a sabot projectile assembly may be loaded separatelybefore each loaded chamber or cartridge is then inserted into, alignedwith, or otherwise securely engaged with the barrel bore (although incertain embodiments or methods of use, loading might take place when thechamber or cartridge is already inserted into, aligned with, orotherwise engaged with the barrel bore). Such a chamber or cartridgemight in certain embodiments provide a housing or support for the sabotdetent or the projectile detent or both. Such a chamber or cartridge mayin certain embodiments have its own bore that substantially matches thebarrel bore caliber and thus may form an extension of the barrel borewhen correctly positioned and oriented relative the barrel bore.Alternatively, such a chamber or cartridge, especially if used toprovide a housing or support for one or more detent means, might besomewhat skeletonized, so as not to include its own section of completebore surface, but rather to provide a housing or support, especially forthe detent means, and which might, for example, be fitted inside thebarrel bore, or fitted into recesses in the barrel wall that possiblycommunicate with the main portion of the barrel bore, or in similarmanners be fitted into an affixed optional mouthpiece or an affixedoptional barrel bore extension member. Such a chamber or cartridge mightin certain embodiments be affixed to the main body of the blowgun insuch a way as to be independently movable of the main body of theblowgun, and thus provide part of an articulated action that could allowloading the sabot projectile assembly by reconfiguring the positioningor orientation of the chamber or cartridge relative the barrel bore toallow the bore or cartridge or chamber to in effect to be opened andloaded, and then reclosed and resealed. Certain embodiments of such anarticulated action might include several such chambers or cartridges,possibly configured to provide a repeater version of the blowgun, suchas a revolver. A multi-chambered embodiment, such as a revolver, mightuse one or more magnetic detents, or in other words might either use onemagnet or a plurality of magnets. Another example of such an articulatedaction might be a break-action embodiment, in which the chamber mighthave its own section of bore matching the caliber of the barrel bore,with the chamber affixed by a connecting means, possibly including ahinge, to the main body of the blowgun in such a manner that in closedposition the chamber's bore would form an extension of the barrel borejoining the barrel bore at the barrel bore breech, while in openposition any hinged articulation of the chamber might allow the chamberto swing down at an angle to the barrel proper, thus opening up whatmight be termed the chamber muzzle. The opened chamber could then bemuzzle-loaded with a sabot projectile assembly and then swung back intoa closed position re-aligned with the barrel bore prior to launching theprojectile. Such a break-action chamber embodiment, the chamber and mainbarrel body might advantageously be provided with gaskets or other meansof providing a secure air seal when the chamber is closed, and mightalso be provided, for example, with additional locking detents adaptedto hold the action closed and sealed until manually or mechanicallyre-opened. It may be appreciated that such a break-action chamberembodiment might make it easier to use a sabot detent embodiment (suchas, for example, a fixed transverse crossbar) which does not allow thesabot projectile assembly to be inserted into the barrel bore throughthe barrel bore breech (or into the chamber bore through the chamberbore breech). Furthermore, in certain embodiments of such a break-actionchamber embodiment, the chamber bore may advantageously have a lengthsomewhat slightly shorter than the length of the sabot projectileassembly, so that when the action is closed, the front portion of theforward end of the sabot projectile assembly rests upon or within theactual barrel bore, in order to reduce any type of jarring or joltingencountered by the projectile assembly when moving across the transitionfrom the surface of the chamber bore to the surface of the barrel bore(in such an embodiment, if the chamber bore were to include a sabotdetent, then the distance between the sabot detent and the muzzle end ofthe chamber would preferably be somewhat shorter than the length of thesabot projectile assembly). In certain somewhat similar embodiments,such a bore extension-type chamber, instead of being hinged to the mainblowgun to form a break action, might instead be completely removablefrom the main blowgun for loading, and then reattachable for launching.

3. Certain embodiments may launch spherical projectiles or other typesof short or non-elongate pellets or projectiles instead of, or inaddition to, launching elongate projectiles.

4. Certain embodiments of the projectile shaft may be tapered or flaredor both at either or both ends as well as in the middle.

5. In certain embodiments the cross-sectional shape of some portion ofthe projectile shaft or foreshaft or both may be other than that of acircular disk shape, which would in some embodiments make it possible,by forming the shaft in a twisted or helical fashion, to provide theprojectile with spiraling surfaces that would aerodynamically inducestabilizing spin. Thus the shaft or foreshaft or both may be shaped insuch a manner so as to provide one or more helically twisted aerodynamicguidance surfaces or other surfaces that produces stabilizing spin inflight.

6. In certain embodiments, the relative positioning and orientation ofany projectile detents and sabot detents relative each other and thebore (especially the breech of the bore) may be other than thepositionings and orientations or relative positionings and orientationsearlier or elsewhere described or depicted.

7. Some embodiments may include both a sabot detent and a projectiledetent, other embodiments may include a sabot detent but not aprojectile detent, other embodiments may include a projectile detent butnot a sabot detent, and yet other embodiments may include neither asabot detent nor a projectile detent. Some embodiments may operate withboth a sabot detent and a projectile detent, other embodiments mayoperate with a sabot detent but without a projectile detent, otherembodiments may operate with a projectile detent but without a sabotdetent, and yet other embodiments may operate without either a sabotdetent or a projectile detent.

8. Certain projectile embodiments, such as the ones depicted in FIGS.1-43, may comprise two or more elements, or in other words may be of atwo-piece or morethan-two-piece construction. Certain alternateprojectile embodiments, on the other hand, may be of a one-piececonstruction. Some such projectile embodiments may be elongateprojectiles, among which certain embodiments may have aforward-of-center balance. In such one-piece elongate projectiles with aforward-of-center balance, the one-piece structure might still beconsidered, if desired, to have a foreshaft portion and a shaft portion,even though the two portions were not structurally or materiallydistinct. A possible example might be an elongate one-piece projectilewith a denser or heavier forward portion that structurally merges into amore lightweight rearward portion. Other one-piece elongate projectilesare possible, however, which might not have a distinguishable foreshaftportion and shaft portion. A possible example might be a one-pieceelongate projectile shaped in the form of an elongate rod, cone, orother suitable shape, and which might be used, for example, simply totest muzzle velocity or target penetration at close ranges, or to belaunched at underwater targets, possibly without concern for in-flightstability past very close ranges. Other possible embodiments for anelongate projectile without distinguishable shaft and foreshaft portionsmight include, for example, a projectile essentially shaped as anelongate rod provided with integrally formed transverse extensionsprotruding from its rearward portion to provide in essence one or morevanes or other types of stabilizing fletching to serve as aerodynamicstabilizers. Some other examples of possible one-piece projectileembodiments include certain embodiments of spherical projectiles andcertain other types of essentially non-elongate projectiles.

9. In certain embodiments, a portion of the foreshaft may servedouble-duty as the head or point of the projectile. Alternatively, incertain embodiments the foreshaft may be adapted or provided with meansto allow the foreshaft to be removably or permanently affixed to any ofa variety of types of structurally or materially distinct projectileheads or points, possibly with one or more intermediary connectingextension members, which preferably would be aligned coaxially with anyhead and foreshaft and shaft. Any such extension members could beaffixed to either the front or the rear of the foreshaft, therefore insome cases possibly overlapping the shaft. Distinct heads or pointswould generally be affixed forwardly to the foreshaft, although somearrangements, particularly one in which the head or point actuallycomprised several distinct elements, might affix to the sides or rearend of the foreshaft (an example might be a head embodiment thatcomprises one or more broadhead blade elements). In certain embodimentsthe portion of the projectile forward the shaft might be considered aseither a foreshaft or a head, so that it would be possible to considerthe projectile as comprising a shaft and head without a foreshaft, orelse simply a foreshaft and shaft; this suggests that in someembodiments the distinction between head and foreshaft might be somewhatarbitrary and the definitions of head and foreshaft essentiallyinterchangeable. Shaft extension members may also be affixed forwardlyor rearwardly to the shaft in order to extend the shaft length, adjustprojectile balance, or possibly to serve as additional aerodynamiccontrol surface or surfaces, depending on the specific embodiment of theshaft extension. Foreshaft extensions might also incorporate additionalaerodynamic control surfaces. The ability or option to affixstructurally distinct heads or points or extension members to theforeshaft or shaft gives the user or designer valuable flexibility inmore precisely adjusting the function, mass, balance, and aerodynamiccharacteristics of the projectile.

10. In certain embodiments a portion of the foreshaft may insert insidethe shaft. Alternatively, a portion of the shaft may inserts inside theforeshaft. Or a portion of each may insert inside or within the other.Or neither may insert within the other. Any inserting, frictional, orforce-fitted engagements between the shaft and foreshaft may be enhancedby means such as, for example, cooperating threads that screw together,glue, or epoxy, or structural means that allow components to snaptogether.

11. In certain embodiments the foreshaft may be hollow for some portionor entirety of its length, and such an inner hollow portion may alsopossibly be open at one or both ends of the foreshaft.

12. In certain embodiments one or more inserts, or outserts, or both maybe added to or affixed to the shaft or the foreshaft or to both, inorder to, for example, adjust projectile mass, or balance, or both.

13. In certain embodiments the sabot detent may engage some portion ofthe sabot frictionally, or by force-fit, or by both, rather thanabuttingly engaging the sabot. Such a sabot detent might possiblyinclude a slightly circumferentially narrower section of bore, or atextured section of bore, or a section of bore that is both textured andnarrowed. In certain embodiments, the sabot detent may function eitherfrictionally or abuttingly, depending on the method of use. In certainembodiments the sabot detent may simultaneously engage the sabot detentat various portions frictionally and abuttingly. In certain embodimentsthe categories of frictional and abutting may overlap, but with one orthe other type of engagement predominating so that the engagement iseither essentially abutting or essentially frictional.

14. In certain embodiments, the blowgun may function without a sabotdetent or may not comprise a sabot detent. In some such embodiments, thesabot piston may be sized and shaped so that the sabot's widest portionfit snugly enough within the bore to frictionally engage the bore insuch a manner as to prevent or resist axial displacements of the sabotprojectile assembly in the direction towards or out the breech. Thistype of frictional engagement with the bore may be enhanced in certainembodiments by an effect in which a backpressure (possibly induced bygravity, magnetic attraction, or mechanical spring bias) of thesubcaliber projectile pressing rearward against its area of engagementwith the sabot causes the sabot to attempt to pivot sideways in thebore, thereby possibly somewhat increasing the sabot's resistance tobackwards motion axially through the bore. In some embodiments ormethods of use, either with or without a sabot detent, the sabot may besized more loosely so as to frictionally engage the bore less securely,yet be held in place or within a suitable range of positions byfrictional engagement of the bore's inner surface, in which case thesabot simply rests on the surface of the bore under its own weight, orin other words under the urging of gravity, especially when the bore isoriented substantially horizontally; in such embodiments or methods ofuse, the sabot generally does not need to support any substantialportion of the weight of the projectile. Adhesion due to breath moisturecondensation in the barrel bore may, in certain embodiments, alsocontribute to the tendency of certain embodiments of the sabot (or theprojectile) to engage the surface of the bore in such a manner so as toresist or prevent excessive premature axial displacement while loadedwithin the bore. It should be noted that in certain embodiments that doinclude a sabot detent, the sabot detent may in some embodiments alsofunction as a primary or redundant anti-inhalation safety means to helpprevent the user sucking the sabot out through the breech. Therefore, inembodiments that do not use or comprise a sabot detent, it is preferableto provide the blowgun with some alternate type of anti-inhalationsafety means.

15. The blowgun in some embodiments, may function without a projectiledetent. One example of such an embodiment is one in which the subcaliberprojectile and sabot means may be held in a suitable loaded positionsimply by their frictional engagement with the bore due to thesubcaliber projectile and sabot each simply resting on the effectualsupport of the inner surface of the bore under the urging of gravity, orin other words by the pressing of their own weight, especially when thebore is oriented substantially horizontally. Thus, in some embodimentsthe blowgun may function either without a sabot detent, without aprojectile detent, or without both. In certain such embodiments, thebarrel bore itself might possibly be considered as being a type ofdetent, possibly either as a projectile detent, or as a sabot detent, oras a combination of both, but the barrel bore will not be actuallytermed as a type of detent in this disclosure for the sake of clarity.

16. Depending on the specific embodiment, the sabot's widest transverseportion or portions may be at either the base or rear end of the sabot,or alternatively, may be positioned transversely at various otherlocations along the axial length of the sabot, including the forward endof the sabot.

17. In certain embodiments such as or somewhat similar to those depictedin FIGS. 1-43, the conical sabot functions, in effect, primarily as apusher plug type sabot component, although the conical sabot may also beconsidered to function somewhat as a sabot carrier in that theengagement of the cone inside the rear opening of the subcaliberprojectile shaft may tend to support some rearward portion of theprojectile above and out of contact with the inner surface of the bore,so that in effect such a conical sabot cone may partially carry thesubcaliber projectile during travel through the bore during launch. Thismeans that the embodiments depicted in FIGS. 1-43 also illustrate orexemplify that in certain embodiments it is not necessary to completelysupport the subcaliber projectile with a carrier type of sabotcomponent, since in certain embodiments the blowgun may function andperform quite satisfactorily with part or all of the length of thesubcaliber projectile resting against and supported directly by thesurface of the bore, without need for the intermediary support of asabot carrier component. It is indeed possible in some embodiments toadapt or orient the subcaliber projectile and the sabot in such a waythat when they are engaged as a functional unit, substantially theentire length, or an elongate portion of the length, of the projectileis in direct contact with and resting upon the inner surface of the borewhen in loaded position and/or during launch. Alternatively, it ispossible in some embodiments to adapt the subcaliber projectile and thesabot means such that some portion of the sabot means functions as asabot carrier that supports the subcaliber projectile in such a way thatno portion of the subcaliber projectile is in contact with the innersurface of the bore while in loaded position and/or during launchacceleration. Such a carrier type of sabot might be most appropriate foruse with a spherical projectile or pellet, particularly if barrelrifling is being used to spin the sabot and transmit spin to the pellet.In such rifled barrel embodiments, the pellet, when in loaded positionand during launching, would preferably be axially centered within thebore, and also preferably aligned with the axial center of the sabot, assubstantially as possible. In such embodiments it would also bepreferable that the sabot and the bore have been pre-shaped in such amanner as to cooperate to produce rifling spin during launchacceleration. Pre-shaping or pre-forming the sabot and the bore toco-operate in such a way would substantially reduce launching resistancewhen compared to the launching resistance that would occur if the barrelrifling needed to grave the sabot during launch.

18. The externally mounted magnetic detent used in the illustrativeexample depicted above in FIGS. 22-43 was not in direct contact, as indirect surface contact, with the subcaliber projectile when theprojectile was in loaded position or being launched. Action or influenceof the magnetic detent upon the loaded projectile was indirect, or at adistance. However, some embodiments may employ a magnetic detent thatdoes have substantially direct surface contact with some portion of thesubcaliber projectile when the projectile is loaded within the bore. Onemethod of employing such a direct contact magnetic projectile detentcould generally be accomplished by providing a receptacle recess or holeinto or through the wall of the barrel, communicating with the bore andpossibly also communicating with the exterior of the barrel. Within sucha receptacle recess or hole may be positioned and possibly affixed someportion of the magnetic detent. Such a receptacle recess or hole wouldessentially transversely extend a portion of the hollow barrel bore.Thus, such a direct contact magnet could be placed into a recessedsocket that opened into the barrel bore, but did not completelypenetrate the barrel wall, if the barrel walls at that portion weresufficiently thick, or the magnet sufficiently small or thin, oralternatively, the recessed socket or hole might completely penetratethe barrel wall. In either such type of embodiment, the top surface ofthe magnetic detent would be preferably aligned and positioned in such amanner that it would not protrude out from the receptacle recess or holepast the inner surface of the bore. The top surface of the magneticdetent might also be shaped in such a way as to match (and possibly becontinuous with and flush with) the curve or perimeter of thecross-sectional shape of the bore where the magnetic detent is located.If necessary a thin surface coating or covering of paint, varnish,plastic, or the like may be applied to any surfaces of the magnet ormagnetic detent which might come in contact with moisture condensationof the breath, or be abraded by surface contact with the swiftlyaccelerating projectile and sabot during launch. Despite any suchintervening protective coating or covering, such a magnetic detent couldstill be understood to be in substantially direct contact with theprojectile when engaged. If the fit of the magnetic detent within such areceptacle recess or hole does not produce a substantially airtightseal, an appropriately sized and shaped gasket might be used to seal anygap between the magnetic detent and the sides of the receptacle recessor hole, or a filler matrix such as some type of epoxy might be usedboth to fill the gap and to affix the magnetic detent in position.Alternatively, a rigid or semi-rigid covering plate or patch could beaffixed to the exterior of the barrel in such a manner as to cover andseal part or all of the external opening of the receptacle hole andthereby seal any gap between the magnetic detent and the sides of thereceptacle hole. Such a covering plate or patch might in someembodiments include a cowl portion shaped and positioned in such amanner as to provide interior clearance for any portion of the magneticdetent protruding from the receptacle hole past the exterior of thebarrel, and to completely cover and seal any opening or gap between themagnetic detent and the sides of the receptacle hole. Such a coveringplate or patch or cowl with interior clearance might result in a smallair space enclosed within the covering, however, provided the airsealremains substantially intact and the volume enclosed by the air space isrelatively small, this need not in any way significantly diminish theperformance of the blowgun. Direct contact magnetic detents could beuseful in situations in which it is needful or desirable to employ amagnet that would not have sufficient strength and dimension of magneticfield to securely attract and hold the subcaliber projectile through arelatively wide range of insertion motion. In such an embodiment, it maybe possible that after initial loading insertion of the subcaliberprojectile, the projectile will be held in initially loaded positionwithin the bore with its rearward shaft end positioned at a distancepast the sabot detent that substantially matches or is only slightlyless than the length of the sabot cone from base to the portion of thesabot cone that directly abuttingly contacts and engages the rear of thesubcaliber projectile. In such embodiments, especially when using asequential method of loading insertion, the user may find it easier toload the sabot in such a manner as to securely engage the sabotprojectile, if the tip of the sabot cone is provided with a narrow,lightweight extension, which is narrow enough that when inserted intoand loosely penetrating the projectile shaft, there is no substantialforce fit or frictional engagement with the inner surface of theprojectile shaft. It may incidentally be noted that in certainembodiments or methods of use the initial partially loaded position ofthe subcaliber projectile is substantially the same or substantiallyalmost the same as the final fully loaded position of the subcaliberprojectile.

It should be noted that another way to provide a direct-contact magneticdetent would be either to use a barrel that includes some structuralportion composed of steel (or some other highly magnetizeable material)with the magnet affixed or held against the exterior of the barrel, orelse to provide a nonmagnetic barrel with a communicating receptacleopening or hole as described above, but with the opening filled orpartially filled with a member of steel (or other suitable magneticallyattractable material), and with a magnet in either direct or indirectcontact with the external end of the steel member, and the projectile insubstantially direct contact with the interior end of the steel member.Using a barrel composed of steel or other magnetically attractablematerial would allow the magnetic detent to be affixed to the barrel bymagnetic attraction without need for any additional connecting meansbetween the barrel and magnetic detent; however, this might generallysomewhat weaken the effectual influence of the magnetic detent upon theprojectile, therefore in many embodiments that utilize a magnetic detentit is advantageous to use a barrel composed of a nonmagnetic ornonmagnetizeable material such as aluminum, plastic, wood, and the like.

It should also be noted that with a magnet not intended to make directcontact with the projectile, or in other words intended to exert itsinfluence indirectly or at a distance, the wall of the barrel could bemade thinner at that portion where the magnetic detent was externallyaffixed or positioned, in order to lessen the distance between themagnet and the magnetizable portion of the projectile, in order tothereby allow a stronger attraction between the magnet and theprojectile.

19. It will be apparent to one skilled in the art that the magneticdetent or other type of detent, and any intermediary connecting meansused to secure or affix the detent in proper position and orientationrelative to barrel and barrel bore, may optionally be so adapted toallow the detent to be, for example, removed or repositioned, orreoriented, and reaffixed or re-secured relative the barrel ormouthpiece. It will be appreciated that if preparing to load and launcha sabot projectile assembly that has a substantially different totallength than the length of the original sabot projectile assembly whichthe blowgun was initially adapted or adjusted to launch, the distancebetween the projectile detent and the sabot detent may need be adjustedor tuned in order to securely hold the current sabot projectile assemblyin loaded position within the bore. (Usually such an adjustment ofdistance between detents may be accomplished by making the projectiledetent repositionable. It would also be possible to make the sabotdetent repositionable, however it is in many embodiments generallypreferable to keep the sabot detent as close to the breech as possiblein order that the sabot projectile assembly be accelerated alongsubstantially the full available length of the barrel bore. Therefore insuch embodiments there would preferably be no need to substantiallyaxially reposition the sabot detent relative the barrel bore. Certainembodiments, however, might advantageously make use of, for example, aratcheting-type mechanism to keep the sabot detent securely biasedagainst the rear of the sabot.)

Any such connecting means to allow adjustment of the positioning andorientation of the projectile detent or other detent might includesimple mounting hardware that could be snapped or screwed to securelybut re-positionably clamp on to the barrel while holding the magnet ormagnetic detent, or could include more sophisticated connecting meansadapted to slidingly affix the magnet or magnetic detent in such amanner as to be continuously or incrementally repositionable along someportion of the barrel, preferably relatively near the breech end orproximal portion of the barrel. In addition to sliding axially back andforth or being axially moved or repositioned to various locations alongthe barrel or along a portion of the length of the barrel, theconnecting means might also make it possible for the magnetic detent tobe reoriented or repositioned in terms of the detent's proximity to theexterior surface of the barrel (thereby also adjusting the detent'slateral distance from the nearest inner surface of the barrel bore), aswell as in terms of the detent's or magnet's tilt angle with respect tothe longitudinal axis of the bore. It would also be possible to provideconnecting means that allow adjustable positioning and orientation ofdirect-contact magnetic detents. Any enlargements in communicatingopenings through the wall of the barrel communicating between the boreand the exterior of the barrel might be externally enclosed by anexpanded cover or cowl that provides adequate clearance for the magnets,mounting and connecting means, and provides a secure air seal.Adjustments of the proximity and orientation of the magnet respectivethe barrel bore allows the user to adjust and tune the strength andorientation of the attractive pull between the subcaliber projectile andthe magnetic detent.

20. In certain embodiments, the projectile detent might also be adaptedas to be repositionable during the loading process in such a way as tohelp it maintain connection with the sabot projectile throughout acertain range of motion of the sabot projectile involved in the loadingprocess. An example would be either a direct or indirect contactmagnetic detent that is slidably affixed to the barrel and is initiallypositioned so as to be attractively engaged by the sabot projectile whenthe projectile is partially inserted into the bore, after which themoveable detent is pulled, by its magnetically attractive engagementwith the sabot projectile, further along the bore or barrel in thedirection away from the breech.

21. The projectile detent might make use of detent means other thanmagnets or electromagnets. Detents could also be used that includedmechanical detents, or even used suction applied through a smallcommunicating opening between the bore and the barrel exterior, forexample. Or possibly a suction or partial vacuum formed behind the sabotmeans and effectually transmitted to the subcaliber projectile by acommunicating opening through the sabot means.

22. The sabot detent, projectile detent or both may be affixed to orintegral with either an optional mouthpiece or an optional affixedextension member that may essentially provide an extended length ofbore, possibly with an integrated mouthpiece portion. In certainembodiments, the projectile detent, sabot detent, or both may be affixedto or integral with an optional sleevelike member that slides over theexterior of barrel and is possibly affixed or secured in place, perhapsslidably or re-positionably. The detent means might also be affixed toor integral with some other type of optional bracket or otherintermediary connecting member or members that is mounted on or affixedto the barrel. Such extension members, sleevelike members, and othertypes of brackets or intermediary connecting members may be adapted toserve as part of an adaptor or conversion accessory or kit for helpingto affix one or more sabot detents, projectile detents, or both, to apre-existing blowgun in order to help convert or adapt the blowgun forlaunching sabot projectiles.

23. In certain embodiments the blowgun may have or be able to accept anoptional barrel bore extension member affixed at muzzle end, breech end,or both (and preferably coaxially aligned with the barrel bore proper).Such bore extension members may use, for example, spring ball detentswith cooperating indentations, possibly with one or more railstructures, to provide a strong connection to and accurate coaxialalignment with the barrel bore proper.

24. In order to increase user convenience in retrieving discarded sabotsafter launching, in certain embodiments the blowgun may advantageouslyinclude an optional sabot catcher means positioned near the muzzle, orotherwise affixed to some portion of the blowgun, and so adapted as toengage and stop the sabot after the sabot exits the muzzle or isotherwise no longer positively by launch thrust. Such an optional sabotcatcher might advantageously be used with a ported bore or boreextension that allows air pressure to drop before the sabot exits themuzzle, and preferably as the sabot approaches fairly near the muzzle,in order to encourage quicker separation of the sabot from thesubcaliber projectile, perhaps even while the subcaliber projectile orsabot is still within or partially within the bore. The bore near or atthe muzzle may also advantageously be somewhat choked or reduced incaliber near the barrel, preferably with a smooth, gradual taper, as anaid in stopping or slowing the sabot, but preferably choked in such away that any portion of the bore that will be in direct surface contactwith the subcaliber projectile is not in any way bent or curved in sucha way as would introduce trajectory inaccuracies by bumping ordeflecting the projectile from the path it has been following down thebore. The optional sabot catcher's structure should be adapted tointercept the sabot means at some point on the sabot's path of travel,preferably at some point on the sabot's external path after exiting themuzzle, but the sabot catcher structure should also preferably notimpinge upon or block any portion of the internal or external path ofthe subcaliber projectile proper and should also preferably notsubstantially interfere with the free flow of air from the muzzle as thesabot projectile assembly pushes a column of air ahead of it down thebarrel during launch acceleration, nor should the sabot catcher, whenengaged with the sabot means during capture of the sabot, substantiallyblock the free flow of residual air flowing from the muzzle after thesabot or sabot projectile assembly exits the barrel bore. The sabotcatcher's structure may include various types of surfaces that areadapted to grip, catch, shunt, frictionally engage, or otherwise engagethe sabot. In certain embodiments, the sabot catcher's sabot engagementsurfaces may, for example, slant inwards towards each other as distanceincreases from muzzle, so as to progressively tighten grip or squeeze inupon the sabot in order to gradually slow or stop the sabot. In certainembodiments, the sabot catcher's sabot engagement surfaces may becomposed of or faced with materials such as, for example, yielding orcompressible foam or foam fingers, flexible bristles, nonskid rubbermaterials. Any such optional sabot catcher structure or mechanism wouldpreferably be so adapted as to not stop the sabot too suddenly, and soas not to substantially block or trap any air flow from the barrel boremuzzle before and after the sabot projectile assembly exits the muzzle.The sabot catcher's sabot engagement surfaces would preferably besomewhat yielding, soft, and smooth, or otherwise adapted in such amanner so as not to excessively abrade the sabot's surface orexcessively deform the sabot or puncture the sabot, thereby helping toextend sabot life. In certain embodiments, part or all of the sabotcatcher may yield during engagement with the forwardly moving sabot, andin certain embodiments part or all of the sabot catcher may moverelative its connection to the barrel or optional stock as the sabotcatcher absorbs momentum and energy transferred from the deceleratingsabot. In certain embodiments the optional sabot catcher may even slideoff or otherwise disconnect from the blowgun proper and fall, possiblystill holding the captured sabot; in certain such embodiments the sabotcatcher might completely disconnect from the blowgun proper and falloff, while in certain other such embodiments the sabot catcher whenmoving or falling might remain movably anchored to the blowgun proper,by, for example, a connecting linkage mechanism, or a string, cable, orchain, by which the main body of the sabot catcher might also beretrieved for surface-tosurface reattachment to the blowgun proper. Incertain embodiments, sliding motion of the sabot catcher engaged withthe decelerating sabot may unlock a spring bias that swings the catcherand captured sabot out of the line of fire in case the user forgets toretrieve or remove the captured sabot prior to launching another sabotprojectile assembly, and also to serve as a more visible visual cue toremind the user to retrieve the captured sabot prior to loading orlaunching the next sabot projectile assembly. In certain embodiments,the optional sabot catcher might also merely slow or deflect the sabot(preferably downward) without completely stopping the sabot, thus merelylimiting how far the sabot travels past the muzzle in order to therebyreduce the work and time for the user to find and retrieve discardedsabots. A sabot catcher catching and retrieving line could even bepermanently attached to a sabot, in a manner similar to the stringattached to the cork in a toy pop gun. A sabot catcher could alsoinclude a loop of string affixed to and trailed by a sabot in such amanner as to engage a hook affixed to the barrel or barrel bore near themuzzle.

25. The optional mouthpiece may be provided with optional intermediaryconnecting means to connect the mouthpiece to the barrel or otherappropriate portion of the blowgun, and in general, optionalintermediary connecting means may be provided to connect together anyappropriate set of elements or optional elements, including accessories,of the blowgun and associated sabot projectiles.

26. In certain embodiments, the subcaliber projectile may be providedwith optional additional aerodynamic fletching in, for example, the formof one or more vanes or feathers, possibly helically wrapped, or in theform of one or more subcaliber cones, cylinders, spheres, disks, or someportion or combination of such shapes or forms. Other means of applyingadditional aerodynamic guidance in certain embodiments might includeoptional projectile surfaces in the general form of a propeller, airscrew, or turbine. Such propeller- or turbine-like surfaces might beaffixed to the subcaliber projectile in order that pressure or lift ofair displaced by the propeller or turbine surfaces would spin someportion or entirety of the subcaliber projectile on its longitudinalaxis. Additional aerodynamic guidance surfaces might also in certainembodiments be grooves or recessed surfaces in or on the projectile,rather than extensions on the projectile. Certain embodiments mightapply additional aerodynamic guidance or stabilizing spin by using anair scoop (somewhat in the manner of a ramjet) to channel displacedpressurized air through exhaust nozzles aligned in such a manner to spinthe subcaliber projectile or some portion of the projectile. Certainembodiments might also use aerodynamic or stabilizing means includingcounter-rotating propeller-like or turbine-like sections rotatingindependently of each other and/or rotating independently of the mainbody of the subcaliber projectile. In certain embodiments in which theprojectile may be hollow throughout some or all of its length, and withany such hollow portion open-ended to allow airflow therethrough, someor all of the inner projectile surfaces may also serve as additionalmeans of aerodynamic stabilization.

27. Rather than comprising a shaft and a foreshaft that are structurallyor materially distinct from each other, the elongate subcaliberprojectile may be formed in one piece, or in other words as a singleunitary monolithic structure, in a number of ways, such as the followingexamples:

a. A one-piece projectile that is wider or thicker at the front than atthe back, so as to create a forward-of-center balance.b. A one-piece projectile composed of certain types of wood, foam, orother suitable materials that may be differentially compressed to yielda permanently compressed structure with the forward section denser andheavier than the rearward section, thereby yielding a forward-of-centerbalance even if the cross sectional dimensions are constant throughoutthe length of the structure after compression.c. A one-piece projectile, either with or without a forward-of-centerbalance, in which additional aerodynamic control surfaces are integrallyformed in the one piece structure by methods such as molding, machining,or carving. An example would be a projectile composed of a dense plasticthat could be molded to form, all in one piece, a relatively thick,rigid, heavy forward body section, tapering down to a thinner, lighterrear body section, with very thin, lightweight fletching vanes extendingradially from the narrow rear portion. Certain types of aerodynamiccontrol surfaces could also be formed by fraying, puffing, or foaming aportion of a relatively solid structure composed of appropriatematerial, such as certain types of plastic and wood.d. Casting, molding, machining, carving or otherwise forming a one-piecemonolithic structure with a solid forward portion and a hollow rearwardportion containing one or more hollow cavities, in which the solidportion serves as a relatively heavy foreshaft portion and the hollowedportion serves as a relatively lightweight shaft portion.e. Rolling a thin layer of material such as plastic film or paper. Anexample would be an L-shaped piece of paper or plastic film rolled sothat one arm of the L would be rolled either inside of, or else aroundoutside of, the rolled-up remaining portion of the L, therebyessentially forming a heavier foreshaft portion, with part of theremaining portion or arm of the L forming a relatively lightweight shaftportion. Another example would be spirally rolling a rectangular stripof plastic film or paper in such a way as to form an elongate cone witha forward-of-center balance due to more layers of film or paper beingrolled at the forward end than at the rear end.

28. Some portion of the subcaliber projectile may, when engaged with thesabot, penetrate an opening through the sabot and extend rearwardly pastsome portion of the sabot.

29. The sabot detent means may be affixed in such a way as to allow itto move relative the barrel or barrel bore. This is particularly usefulin embodiments in which the subcaliber projectile, after being loadedinto the initial partially loaded position, is further inserted only arelatively small distance to assume final completely loaded position, orelse in which the initial loaded position of the subcaliber projectileis also substantially its final loaded position. In this case, sincethere may in some such embodiments not be any substantial backfollowingmotion, as described above, to keep the projectile securely followinglyengaged against the sabot, being able to move the sabot detent forwardafter the sabot has been inserted past the sabot detent helps to ensurethat the sabot and subcaliber projectile are firmly seated against eachother, or in other words firmly abuttingly engaged. Such a followinglymovable sabot detent means might in some embodiments be provided with aratchet type mechanism in order to help prevent slackening or looseningof pressure or contact against the sabot. Such a moveable sabot detentmay advantageously be used in conjunction with sabots provided withslender tip protrusions or other similar provision adapted to slide veryloosely either into or around (or both) a portion of the projectile inorder to thereby guide the main portion of the sabot and the subcaliberprojectile together or back together after any axial separation that didnot exceed the length of the tip protrusion, and to thereby give anextended buffer zone to help provide more resistance to premature orexcessive lateral dislocation of the sabot relative the projectile.

30. In certain embodiments, the projectile shaft need not necessarily beof constant inner diameter or outer diameter. On the other hand, incertain embodiments the projectile foreshaft may, for example, be ofconstant diameter, or may have a forward portion narrower than arearward portion, or may be shaped in an essentially non-cylindricalfashion, such as, for example, a foreshaft shaped in an essentiallyconical or cylindroconical fashion.

31. In certain embodiments the sabot may be provided with means topartially or completely encapsulate the subcaliber projectile. Oneparticularly useful version of such a sabot could include a pusher plugsection rearwardly affixed to one or more forwardly extendinglongitudinally aligned elongate members that are substantially as longas or longer than the projectile. If the sabot included two or more suchlongitudinal elongate members, then each member could include aprotrusion extending radially inward from the forward end of the memberso that the radially aligned protrusions would meet or overlap, in amanner similar to upper teeth meeting lower teeth in the mouth. Whenclosed together or against each other, the radial protrusions mightcombine to define a forward partition or socket that in cooperation withsome portion of the pusher plug may longitudinally encapsulate theprojectile abbuttingly. The longitudinal members or radial protrusionsor both may be pivoted, hinged, or flexible so as to be able to spreadapart, when not constrained by the transverse dimensions of the bore,and thereby release the forward end of the projectile so that sabotdiscarding may occur. Additionally or alternatively, the radialprotrusions might be independently compressible or resilientlycompressible and able to spread apart to release the projectile withoutrequiring the longitudinal elongate members to spread apart. Thelongitudinal elongate members or radial protrusions might in certainembodiments also be provided with or linked to additional forwardextensions adapted to exit the muzzle and be pushed apart laterally byatmospheric drag, thereby helping to disengage the linked elongatemembers or radial protrusions from contact with the forward end orportion of the projectile before the sabot has completed exiting fromthe muzzle. If only one lateral elongate member is used, it could beprovided at its forward end with a transverse protrusion that would abutthe inner surface of the bore in order to define a forward containmentpartition or socket to cooperate with some portion of the pusher plug topartially encapsulate the projectile, especially if the forward end ofthe projectile rests on or is pressed against the inner surface of thebore. The forward protrusion or protrusions would not have to beactually abutting with each other or with the bore, but simply closeenough together or close enough to the bore so that the remaining gapwould be too narrow for the forward end of the projectile to slidethrough, so that there would still be secure abutting forward engagementof the projectile. A parallelogram type linkage could be used to allowaxially forward motion of the projectile to essentially transverselymove or swing the forward sabot extension or protrusion out fromdirectly in front of the forward end of the projectile.

32. In certain embodiments, some portion of the projectile other than,or in addition to, some portion of the projectile foreshaft, maycomprise a magnetically attractable portion to cooperate with a magneticdetent. In certain such embodiments, then, the projectile foreshaftmight not include any magnetically attractable portion.

33. In certain embodiments, a magnetic detent may also be furtherutilized to hold one or more magnetically attractable projectiles withineasy reach on the exterior of the blowgun. In certain such embodimentsor similar embodiments, the sabot might also include a magneticallyattractable portion, such as a lightweight strip of the type of tapeused in tape recorder cassettes, to allow the sabot to be held by amagnetic detent on the exterior of the blowgun.

34. Rather than using a magnetic detent containing one or more magnetsthat attracts some magnetically attractable portion of the projectile toconfine the projectile in loaded position, alternatively the projectileitself might contain one or more small magnets, while the blowgun propercontains some magnetically attractable portion. Or both the projectileand the blowgun may each contain one or more actual magnets, which mighteither attract or repel each other, according to the specificembodiment, in order to confine the projectile in loaded position.

35. It was noted earlier above that certain embodiments may utilize anelectromagnetic detent means. Certain embodiments that include anelectromagnetic projectile detent may be substantially identical with orsimilar to embodiments that use permanent magnets, but with the simpleexception that the permanent magnets are merely replaced by suitablyadapted electromagnets that may in certain embodiments be substantiallysized, shaped, positioned and oriented, and possibly re-positioned andre-oriented adjustably, much as the permanent magnets were in variousembodiments (in such embodiments, each electromagnet might typicallyhave its own specialized core element distinct from the other elementsof the embodiment). In certain other embodiments, however, theelectromagnet might utilize a portion of the blowgun barrel itself as acore, provided the barrel or suitable portion of the barrel is composedof a suitable material to serve as an electromagnet core. Embodimentsare also possible in which a magnetically attractable portion of theprojectile might serve as a core or movable core for an electromagneticdetent, which might possibly thus resemble a type of electromechanicalsolenoid, especially if the induction coil were wound around a portionof the barrel (or might alternatively possibly resemble a simplerelectromagnet if the induction coil was wound directly around a portionof the projectile). Thus various embodiments are possible in which theinductive coil of the electromagnetic detent may be wrapped around aportion of the barrel, in order to thereby in certain embodiments usethe barrel portion itself as a core, or in other embodiments use themagnetically attractable portion of the projectile as a movable core.Other embodiments are also possible, in which the inductive coil of theelectromagnetic detent might be wrapped around a core element other thana portion of the barrel or portion of the projectile, thus substantiallyresembling in many ways certain embodiments that include permanentmagnetic detents. However, embodiments that include the various types ofelectromagnetic detents do offer certain possibly unique advantages andadditional features appropriate for certain situations and methods ofuse. A list of some of the advantages and features of embodiments thatinclude electromagnetic detents includes:

a. The electromagnetic detent's magnetic field may in certainembodiments be able to be switched off, either manually orautomatically, when the blowgun is not in use. This might be convenientwhen storing the blowgun near items that would be sensitive to a strongmagnetic field.

b. Certain embodiments may include means for manually or automaticallyadjusting or varying the strength of the electromagnetic detent'smagnetic field, in order to make it easier to fine tune blowgunperformance or initial launching resistance for example. Means mightalso be included that allow variation or adjustment, possiblyautomatically, of the electromagnetic detent's magnetic field strengthduring various stages of the loading and launching sequence.

c. Certain embodiments might include means for automatically switchingon electric current to the electromagnetic detent upon insertion of themagnetically attractable portion of the projectile within an appropriateportion of the barrel bore. Certain such embodiments might, for example,use the attraction of a small permanent magnet to the projectile'smagnetically attractable portion in order to switch on the flow ofcurrent to the electromagnet.

d. Certain embodiments might include means for automatically switchingoff electric current to the electromagnetic detent at some point duringlaunch acceleration, or after the completion of launch acceleration, oreven just prior to launch acceleration. Such embodiments might, forexample, utilize electric switching means possibly actuated by changesin air pressure during launch, or possibly actuated by inductanceeffects or magnetic attraction between the accelerating projectile andthe electromagnet or electromagnetic coil. Use of an in-line pressurerelease valve to temporarily block the air passage through themouthpiece, breech, or bore, as described earlier above would provideone way of allowing a pressure sensitive switching means to be actuatedby launch pressure and cut current to the electromagnetic projectiledetent somewhat slightly before the actual commencement of launchacceleration.

e. Certain embodiments might allow for physical repositioning andreorientation of the electromagnetic projectile detent relative the boreand relative the sabot detent in order, for example, to accommodateprojectiles or sabot projectile assemblies of varying lengths. On theother hand, embodiments would also be possible in which such adjustmentsfor varying sabot projectile assembly lengths were made by selectivelyenergizing one or more of various sequentially positioned electromagnetsaffixed in relatively immovable or permanent positions along the barrelor barrel bore, or by selectively energizing one or more portions of thecoil of a single extended electromagnet so that only a portion ratherthan the total of the electromagnet's length is energized or generatinga magnetic field.

f. In certain embodiments the electromagnet or the electromagnet's coilmight itself form a portion of the body or wall of the barrel, or of abarrel bore extension member, or of a mouthpiece (preferably with asuitable protective coating or sealant applied to the electromagnet).

36. In certain embodiments, rather than including a magnetic projectiledetent, the embodiments may include various types of essentiallynon-magnetic projectile detents, such as, for example, various types ofdirect-contact mechanical projectile detents. It will be apparent to oneskilled in the art that suitable positioning and orientation ofmechanical projectile detents or other nonmagnetic projectile detentsrelative the barrel bore and relative the sabot detent willsubstantially follow, perhaps with certain modification or adjustment,the essential principles or considerations, set forth earlier, forsuitably positioning or orienting a magnetic projectile detent relativethe bore and relative the sabot detent (as well as any considerations oradjustments necessitated for example, by affixing detent elements to acartridge, chamber, mouthpiece, or bore extension member, rather than tothe barrel proper or barrel bore proper of the blowgun). A few briefexamples are listed below to serve to illustrate some of thepossibilities for such mechanical projectile detents, and may suggestnumerous alternative embodiments or versions to one skilled in the art:

a. One type of preferred embodiment including such a mechanicalprojectile detent would also include a straight longitudinal guidancegroove in the inner surface of the barrel bore, as described above (orpossibly with some other type of groove or recess in the bore). Such amechanical projectile detent might comprise, for example, one or morehinged or flexible fingers affixed within and extending transverselyacross some portion of the guidance groove, with the finger or fingersinternally or externally biased yieldingly towards a resting position orinitial position partially or completely transversely obstructing theguidance groove. The forward end of the projectile or projectileassembly, or other appropriate projectile portion adapted tocooperatingly engage the guidance groove, may, when in loaded positionwithin the bore, rest in the groove and abuttingly rearwardly engage themechanical detent finger or fingers. The detent finger or fingers may beadapted to partially yield when the projectile is being inserted intoloaded position, but once loading insertion is complete, the detentfinger/s should preferably still abuttingly engage the front end of thecooperating portion of the projectile with sufficient firmness toprevent or resist premature excessive forward axial displacement of theprojectile prior to launch acceleration. The detent finger or fingersshould preferably also be adapted to yield readily enough to be readilypushed aside when the projectile forcefully moves forward during launchacceleration, or in other words the initial launch resistance imposed bythe detent finger/s should preferably be able to be readily overcome bythe operating pressures provided by a typical human user's breath. Theadvantage of positioning, orienting, and otherwise adapting themechanical projectile detent to partially or completely transverselyobstruct the guidance groove and thereby engage some portion of theprojectile that cooperates with the guidance groove, is that after thecooperating portion of the projectile has pushed past the mechanicaldetent during launch acceleration, the remaining portions of theprojectile and of any sabot means can pass by through the barrel boreproper, thereby avoiding any contact with the mechanical projectiledetent (this of course assumes that the mechanical projectile detent isadvantageously so adapted that no portion of the mechanical projectiledetent protrudes out of the guidance groove, or otherwise protrudes intoor across the barrel bore proper). It will be apparent to one skilled inthe art that such a mechanical projectile detent within a guidancegroove in the barrel bore might, rather than comprising detent fingers,instead comprise other types of extensions, protrusions, or othersuitable means to partially or completely transversely obstruct theguidance groove and thereby engage and hold the projectile when inloaded position. It would even be possible for such a projectile detentwithin a guidance groove to simply comprise a transversely narrowerportion of guidance groove that could engage the cooperating portion ofthe projectile in an abutting, frictional, or mildly force-fittedmanner, depending on the particular embodiment.

b. Certain embodiments that comprise a mechanical projectile detent orother nonmagnetic projectile detent may have portions of the projectiledetent which protrude into or across the barrel bore proper, especiallywhen the projectile is in loaded position and engaged with theprojectile detent. Such embodiments may or may not have a guidancegroove in the bore, but are perhaps more likely to occur when there isno guidance groove. In such embodiments, the mechanical projectiledetent might, for example, comprise a gripper element that transverselysnaps on and off some portion of the projectile, or that inserts intoand snaps into or frictionally engages a portion of the projectile, orthat wraps around a portion of the projectile (this last might possiblyinclude an element such as a piece of string that could be configured asa type of slip knot or sliding loop that could slide open or release asthe projectile moves forward during launch). Any such projectile detentelements that protruded into or across the bore proper might, in certainembodiments, be so adapted or provided with means so adapted as to bebiased in such a way that when the cooperating portion of the projectilereleased from the detent's hold or engagement, the protrusive portionsof the detent could retract into a hole or recess through or in thebarrel wall in order to clear the bore and substantially avoidengagement with or obstruction of the remaining or trailing portions ofthe projectile and any sabot means. In certain embodiments any suchprotrusive projectile detent elements might alternatively simply beadapted to either yield under contact with any portions of projectile orsabot means, and preferably be yieldingly pushed back into cooperatingrecesses or holes in the barrel walls, or alternatively any suchprotrusive projectile detent elements might simply be sized, shaped,and/or otherwise so adapted as to let any contacting portions of theprojectile or sabot means to ride over the protrusive detent elementsfairly smoothly. Certain embodiments in which portions of the projectiledetent retracted into openings or recesses in the barrel wall mightadvantageously be provided with a push button or other means suitablylinked to the retractable detent elements in order to allow the detentelements to be reset to suitable positioning and orientation to engagethe next projectile loaded into the bore.

c. Certain embodiments may use a mechanical projectile detent thatinserts through a longitudinal opening pierced in a sabot to therebyengage some portion of a projectile. An illustrative example might be ablowgun provided with a transverse crossbar removably affixed across thebreech opening, with the crossbar provided at its substantial centerwith a forwardly extending, slender metal or plastic protrusion,advantageously resiliently flexible, and preferably substantiallynarrower than the inner diameter of the projectile shaft's rear opening(assuming use in this embodiment of a projectile similar to the one usedin the embodiment depicted in FIGS. 1-21.). The rear end of theprojectile shaft might advantageously be plugged with a small piece offoam rubber or other suitable material force-fitted into the rear end ofthe shaft. The sabot means might advantageously be a conical shell sabotwith a small hole pierced through the sabot tip, with the holepreferably just large enough for the crossbar protrusion to fit through,yet with the hole small enough that the sabot structure would still beable to securely abuttingly and loosely penetratively engage the rearend of the projectile shaft (in other words, so that the cone tip wouldnot be overly weakened and collapse, or so that the cone's tip holewould not be so large that the shaft's rear end could slip into orthrough the sabot hole). To use this embodiment, the user could removethe transverse crossbar from the breech end of the barrel and insert theslender crossbar protrusion, which might advantageously have a somewhatsharp point, through the tip opening of the conical shell sabot andtherethrough push the slender protrusion into the rear end of theprojectile shaft to somewhat firmly penetratively engage the foam plugwithin the projectile shaft. The user could then preferably push theprojectile back to firmly seat the projectile's rear end against thesabot, and also seat the sabot's rear end against the main body of thetransverse crossbar. The user could then insert the projectile assemblyinto the barrel bore and re-attach or re-affix the transverse crossbaracross the breech opening of the bore. During launch acceleration,launch thrust may push the projectile and sabot forward so that theprojectile and sabot slide completely off of the slender protrusion, andso that the slender protrusion releases its penetrative engagement withthe foam plug or other portion of the projectile or sabot, and theprojectile and sabot are thereafter free to separate freely aftercompleting launch exit from the muzzle.

d. Certain embodiments that include a mechanical projectile detent mightinclude a frangible detent element that may be torn, broken, or cut inorder to release the projectile during launch, and in particular withthe frangible element weak enough to be broken by operating pressuressupplied by human lungs. An example might be a paper loop that is loopedaround some portion of the projectile and is affixed to the barrel orbore, with the loop materially composed and structured and otherwise soadapted so as to be able to be broken, torn, or cut by the push of theengaged portion of the projectile as the projectile is pushed forwardduring launch.

e. Certain embodiments might include different types of nonmagneticprojectile detents than those listed or suggested above. For example,one type of nonmagnetic projectile detent, which might incidentally beconsidered to operate without direct mechanical contact with theprojectile, might be a projectile detent that utilized suction or apartial vacuum applied to the projectile (and possibly also to thesabot) through one or more communicating holes or passages through thebarrel wall, or possibly through one or more communicating holes orpassages through the body of the sabot means (actually, such a suctionaldetent could be used to provide either a projectile detent means or asabot detent means or both). For example, a suction bulb or piston couldbe affixed externally to the barrel wall, with the bulb or piston airchamber linked to one or more holes or air passages through the barrelwall. One or more appropriate cooperating portions of the projectile (orsabot, as appropriate) could be positioned against the inner surface ofthe bore and above the appropriate air passage opening or openings inthe bore. The user could then manipulate the bulb or piston to introducea suction or partial vacuum into the air passage holes and thereby suckand seal some portion of the projectile or sabot against the innersurface of the bore over the air passage opening/s in the bore. Thestrength of the suctional hold on the projectile or sabot shouldpreferably be suitable to operate compatibly with the range of operatingpressures provided by human lungs so that the user's breath couldovercome and break the detent's sectional hold on the projectile orsabot. It would also be possible in certain embodiments to use valvesand perhaps additional air passages in order to allow the user's breathduring launch to directly fill the detent vacuum and thus actuallysubstantially eliminate the detent's suctional hold on the projectile orsabot.

37. Certain embodiments of my invention may include one or more optionalin-line pressure-release valves across or within or opening into thebarrel bore at the breech or muzzle or both, or possibly also oralternatively positioned elsewhere along or within the barrel bore. Oneor more such valves could also or alternatively be positioned within anoptional mouthpiece or optional bore extension member affixed to theblowgun barrel. An illustrative example of such an embodiment couldinclude such a pressure-release valve housed within a mouthpiece affixedto the blowgun barrel. In this exemplary embodiment, an intermediaryportion of the mouthpiece's hollow interior passage could be acube-shaped void or chamber, which would have four square sides, and twosquare end openings, and the pressure-release valve could comprise ahinged flap so sized and shaped as to substantially match the size andshape of one of the square end openings of the cubical void or chamberin the mouthpiece. The square valve flap could be hinged at one edge tothe body of the mouthpiece (with the flap preferably hinged to themouthpiece body at the lip of the square end opening closest to the airinlet end of the mouthpiece), in such a manner that the valve flap couldswing down to a closed, transversely-aligned orientation in order tothereby substantially completely obstruct and seal the cubical chamber'ssquare end opening closest to the air inlet end of the mouthpiece, andwith the valve flap also hinged and positioned in such a manner that thevalve flap could swing up within the cubical chamber to assume an open,longitudinally-aligned orientation substantially flat against one of thesides of the cubical chamber in order to thereby allow a substantiallyunobstructed flow of air through the cubical chamber. The mouthpiecebody would advantageously also have one or more extensions, affixed toor integral with the mouthpiece's inner surface, and positioned at ornear to one of the edges of the cubical chamber's square-shaped openingthat is nearest the air inlet end of the mouthpiece, with any suchextensions sized, shaped, and otherwise so adapted to abbuttingly orotherwise engage the valve flap in order to prevent or resist the flapswinging past the position of substantially transverse alignment thatwould provide the best obstruction or seal of the square chamberopening. Such an embodiment might also advantageously have some portionof the valve flap composed of a substance strongly susceptible tomagnetic attraction, and have a magnet affixed to or within the mainbody of the mouthpiece, with the magnet positioned and oriented in sucha way as to exert substantial magnetic influence on the susceptibleportion of the valve flap when the flap is oriented in its closed,transversely sealing position, with the amount of magnetic attractionbetween the magnet and flap still readily overcome by the breathpressure of the user. To use the blowgun provided by this embodiment,the user could insert the projectile or projectile assembly through themouthpiece, with the projectile or projectile assembly pushing the flapup to an open position during loading, with the flap able to swing backshut after the projectile or projectile assembly has been pushed past itand finger or optional insertion tool withdrawn (the flap might swingshut under gravity, or attraction to the magnet, or an internal orexternal spring balance, or some combination thereof). An optionalinsertion tool or mechanism might make it easier for the user to pushthe projectile into loaded position. When the'user blows into the airinlet end of the mouthpiece to initiate launch, the flap wouldpreferably be held momentarily in place by the magnet, before thepressure of the user's breath overcame the hold of the magnet on theflap and forced the flap into open position. Thus such a valve couldallow higher launch pressures or earlier peaks in launch pressures todevelop. It will be recognized that this is similar to the detent delayeffect that may be produced as a result of using a projectile detent incertain embodiments. Such a pressure-release valve or valves could beused either in conjunction with a projectile detent or else without aprojectile detent, depending on the particular embodiment, and due tothe higher launch pressures or earlier peak pressures that may develop,such embodiments that include one or more pressure-release valves mayachieve higher launch velocities when used either with sabot projectilesor with fixed-piston full caliber projectiles. Any pressure-releasevalve located between the projectile or projectile assembly and themuzzle opening of the bore (or located at the muzzle opening) may alsoachieve a similar effect, since the column of air trapped between theprojectile piston or sabot will keep the projectile or projectileassembly essentially immobilized until pressure builds sufficiently torelease the valve flap from the magnet's hold. It will be apparent toone skilled in the art that numerous alternate embodiments of such apressure release valve are possible, and that certain such embodimentsmight use, for example, a mechanical latch rather than a magnet to holda flap or other valve portion in sealed position.

38. Certain embodiments may include a multi-stage sabot or sabot, whichmay possibly be adapted for transition between two or more sections ofbore with differing calibers.

39. When using a blowgun, muscular effort of the user and compressed airfrom the user's lungs provide the energy to launch the projectile. It isadvantageous, therefore, to very carefully match or adjust particularweapon variables to particular user variables in a way that issubstantially individually customized. With the blowgun, some majorweapon variables are bore caliber, barrel/bore length, projectile mass,projectile sectional density, and projectile form factor. Also to beconsidered is whether overall dimensions will be comfortable or awkwardfor a user to hold and engage with the mouth (as well as the fit of themouthpiece itself). For example, a typical young user may not haveenough lung capacity to use a relatively large-bore, long-barreledblowgun. Likewise, projectiles of a given mass may be too heavy for atypical young user to propel without undue strain and poor velocity. Inthis case, a blowgun with a relatively medium or small bore, with ashort or medium length barrel, and relatively lightweight projectilesmight be indicated as preferable for helping a typical young user toachieve improved results, and if the lightweight projectiles happen tobe of relatively low sectional density, perhaps due to being fullcaliber fixed-piston projectiles, it might also be indicated orrecommended that such projectiles be used at close range to offset thelow sectional density. On the other hand, lightweight subcaliberprojectiles might be adapted to have relatively high sectionaldensities, with correspondingly increased effectiveness at longerranges.

A perhaps subtler but still relevant example of considerations whenattempting to match blowgun characteristics with individual usercharacteristics or preferences: Consider either an adult user or a younguser with sufficient lung capacity and muscular strength carry, handle,and otherwise make efficient, controlled use of a blowgun with arelatively large bore and long barrel. Generally speaking, many usersmay not be willing to use the strictly optimal or maximum barrel length(for achieving maximum projectile velocities or increased accuracy) ofwhich they are technically capable of handling and using, because theymay feel that an excessively long barrel is awkward to use and carry, orhard to store. Therefore it is advisable, at some point in thecustomization process, to determine the maximum barrel length the userwants to use or is willing to use (barrel extensions may be used toextend or adjust barrel/bore length in certain situations).

User preferences may also possibly differ or change according to theintended application or method of use. For example, target shootingpreferences and hunting preferences may possibly differ from each otherin that hunters generally wants to deliver as much energy as reasonablypossible to the target, in addition to delivering a projectile withreasonable accuracy, while target shooters on the other hand may perhapsbe interested only in maximizing accuracy.

Following is a list of considerations or tests which may help tocustomize blowgun and projectile characteristics for improvedperformance with a particular individual user:

*Measure lung capacity volume by user. Possibly test lung pressure orbreath pressures developed as well.*Determine any limiting factors such as user preference, or comfort orability in handling, that may place additional limits on how long thebarrel or bore may be.*Use the above to narrow down to an initial range of preferable boresizes (length and caliber). For a different barrel or bore lengthoptimal bore caliber may change.*Test user's performance with each preferably bore size with incrementsof dart mass, measuring muzzle velocities with chronograph or otherappropriate instrument. Also monitor user's subjective comfort levels.*Provide a trajectory map for each bore+length+dart mass+formfactor+sectional density+ballistic coefficient. Set up a default idealsight template.*Optimal projectile balance also to be considered and systematicallytested.*Initial launching resistance and detent delay effect, includingpossible subjective reactions or flinching on the part of the usershould be considered.*Preferable to let the user “warm up” first with “neutral” ornon-customized average specimens of blowgun and projectiles in order tohave more of an informed basis for gauging performance and comfortimprovements with various customized or tuned adjustments.

Once matching of optimal bore, barrel length, and projectile mass forthe particular user and particular method of use or application has beendone, optimal form factor and sectional density of projectiles,especially subcaliber projectiles, can be calculated. Idealtrajectory/projectile paths could be plotted out to desired range (say,up to 50 yards for example) and corresponding sighting or targetingreticles (or other sight devices) could be printed or configured.

The probable tendency of some shooters to eschew long barrel lengths,say, for convenience of handling or storage, may be offset by somedegree by the option to increase bore caliber and decrease projectilemass, within practical limits, while still being able to achieve goodsectional density levels, possible with certain embodiments that usesubcaliber projectiles.

Lung capacity, strength and conditioning of relevant muscle groups, andtechnique in utilizing said capacity and strength, are all part ofdetermining how effectively a particular user is able to use a givenblowgun and projectiles. With a blowgun, propulsive thrust is suppliedessentially by the user's lungs and diaphragm. Each user will have acertain lung capacity, with a certain portion of that lung capacity ableto be utilized to produce thrust, and a certain amount of strength,stamina, training, and skill in the relevant muscle groups to producethrust and to achieve stable balance, handling, aiming orientation andthe like. Accordingly, some users may have limits on the length andweight of barrel they can manually handle and aim proficiently. Withouttaking these variables into account, many users will, even ifunwittingly, be matched with a blowgun and projectiles that are anactual handicap. Comfort level and velocity may preferably be optimizedin tandem with regard for both rather than for just one. When usingsubcaliber projectiles, it may be easier for undue user strain to beavoided, since somewhat lower velocities may still yield goodtrajectories.

It is preferable that various methods of matching, customizing, oradjusting will be provided so that the user may either use somewhathigh-tech routes or somewhat low-tech routes to get a good match orachieve good tuning.

Some of the weapon variables that may be adjusted or customized, tuned,or otherwise personalized to optimize an individual's performance andcomfort include:

*Air volume or displacement volume of the barrel bore (a function ofbore caliber and bore length).*Barrel length, Bore Caliber, and Bore Length.*Projectile mass, balance characteristics, and configuration ofaerodynamic surfaces.*Projectile form factor matched to anticipated range of velocities,anticipated methods of use, and projectile mass.*Snugness of fit within the bore of the projectile piston or sabotpiston.*The strength of the initial launching resistance and of any detentdelay effect.*Frictional coefficients of projectile assembly components in surfacecontact with the bore, and of the bore itself.

40. Certain embodiments of my invention may utilize means for providinga positive connection between the subcaliber projectile and the sabotmeans, in which the positive connecting means may be considered asactually being an integral component or set of components of the sabotprojectile assembly, and as such, in some embodiments may also undergolaunch acceleration or discarding. An illustrative example of anembodiment which includes such positive connecting means may be obtainedby somewhat modifying or adapting a sabot projectile assembly similar tothe one depicted in FIGS. 22-43. The user could even make certainembodiments of such a modification or adaptation connecting means byhand, although it will be apparent that essentially equivalentmodification adaptations could be manufactured by commercial processes.For convenience of illustration or description, it will be assumed thatin this case the subcaliber projectile has been made by hand from atruncated finishing nail foreshaft, and a plastic sipper/stirrer strawshaft (as was described in more detail elsewhere). To hand-make such amodification connecting means, the user could take a short section(perhaps 1.5 inches long, more or less), of another sipper/stirrer strawand split (slit both sides of) the straw section lengthwise for all butabout one-half or one-quarter inch of the length at one of the ends ofthe section. By trimming the two half-sections along the length of thesection that was split, the user may make two strips or arms that extendfrom the short unsplit section, with the strips or arms preferablyedge-to-edge along one of the original slits, with the opposite originalslit having been widened by trimming. Preferably each strip or arm wouldbe trimmed so as to appear essentially flat. The user may now take theshort, heretofore unsplit section and slit it along one of its sides(preferably the side opposite the side with the unwidened original slitbetween the two arms that were already made). It will likely beadvantageous to widen the slit in the short section by trimming alongits edges, until the short section may fairly easily be transverselysnapped onto and off of the straw shaft of the subcaliber projectile.The resilient flexibility of the sipper-stirrer straw material willallow the slit short section to spread apart and snap onto and off ofthe projectile shaft, and will also allow the two arm sections to bespread apart somewhat. The two arm sections can then be spread apart andaffixed, possibly with tape or glue, one on each side of the conicalshell sabot. The arms should preferably be affixed in such a manner thatwhen the short section is snapped onto the projectile shaft, and thesabot tip is inserted into and engaged with the rear end of theprojectile shaft, the arms fastened to the sabot will constrain thesabot to rest at somewhat of an angle to the longitudinal axis of theprojectile shaft. Thus the arms and short section together form astructure rather like a yoke or harness, with the spread-out position ofthe arms helping to add some rigidity to the arms. When loading such asabot projectile assembly, the user may start with the sabot projectileassembly fully assembled and snapped together with the short section ofthe yoke snapped onto the projectile shaft in order to hold the sabotand projectile engaged together. The user may insert the sabotprojectile assembly partially into the bore and allow the magneticdetent to hold the sabot projectile in place against the inner surfaceof the bore in partially loaded position. The user may then manuallytilt or rock the sabot to the opposite side of its original tilt, insuch a manner that the sabot tip stays within the rear end of the shaft,and the tension of the sabot being tilted to the opposite side causesthe short yoke section, pulled by the yoke arms, to transversely snapoff of the projectile shaft. The user may now complete manual insertionof the sabot projectile assembly, in which the positive connecting yokemeans has now been disengaged, and continue to launch in the mannerdescribed in FIGS. 22-43. It will be apparent to one skilled in the artthat numerous versions similar to this embodiment are possible, with,for example, less or more yoke arms, or other differences, and thatthere are numerous other embodiments possible which use differentspecific means to allow a snap-on/snap-off positive connection, or atwist-on/twist-off connection, or various other types of connectionsbetween the sabot and the projectile, or which might be used with otherspecific embodiments of the sabot and projectile than those embodimentssimilar to the ones depicted in FIGS. 22-43.

41. The sabot may in some embodiments be provided with a port hole orother air passage means in order that during launch compressed air maypass through the sabot port hole or air passage to enter into andcollect within the hollow shaft or other internal air spaces definedwithin the body of the projectile in certain embodiments, so that afterdiscarding of the sabot means, the compressed air would expand and flowback out the back opening of the hollow shaft or air space, therebypossibly generating a base bleed effect to reduce vacuum behind themoving projectile and possibly increase aerodynamic stability of theprojectile, or possibly serving as a means to disperse a powder oraerosol for a tracer projectile effect.

42. The projectile detent may in some embodiments be positioned alongthe barrel between the sabot detent and the breech, or even affixed to amouthpiece or bore extension member and therefore possibly beyond thebreech (and therefore not along or overlapping the barrel). The sabotdetent may also be affixed to the mouthpiece or a bore extension member.If both the projectile detent and the sabot detent are affixed to themouthpiece, the projectile detent may in some embodiments be positionedcloser to the air inlet end of the mouthpiece than is the sabot detent.

General Principles, Conclusions, Ramifications, and Scope

The prior-art obstacles to utilizing sabot projectiles in blowguns,presented in the foregoing discussion, may be substantially eliminatedby employing a sabot projectile adapted to operate efficiently at theoperating pressures and velocities typical of blowguns and associatedprojectiles. More specifically, this may be made possible by using sabotprojectiles and blowguns so adapted as to greatly minimize projectileassembly launching resistance and sabot discarding resistance, yetpreferably also so adapted as to prevent premature axial or lateraldislocation of the sabot projectile components relative each other andrelative the barrel bore prior to launch acceleration and exit from thebarrel muzzle. Thus in many embodiments it is important, for thepurposes of securing the sabot projectile components as a functionalunit during certain stages of the loading and launching sequence, and ofmaintaining the loaded sabot projectile assembly unit in proper positionrelative the barrel bore prior to launch acceleration, to employ suchmeans as are preferably adapted to substantially eliminate or greatlyreduce the use of positive connecting means, force fit, frictionalengagement, and the like, and which are preferably further so adapted asto ensure that after the sabot projectile assembly has exited the barrelmuzzle and propulsive thrust has dissipated, there is substantially nopositive connection between the subcaliber projectile and the sabotmeans, either directly or via intermediary connecting means, which wouldprovide any substantial resistance to axial displacement of thesubcaliber projectile forwardly relative the sabot means, nor to axialdisplacement of the sabot means rearwardly relative the subcaliberprojectile. Thus any direct positive connection that may exist betweensabot and subcaliber projectile, either directly or via intermediaryconnecting means, during earlier stages of handling, loading, orlaunching, should preferably have been disengaged or disconnected priorto the completion of exit from the muzzle by the sabot projectileassembly.

I have accordingly determined that launching subcaliber projectilesefficiently and accurately from a blowgun can be accomplished in certainembodiments of my invention by adapting the blowgun and associatedprojectiles and sabots according to one or more of the principles andmethods detailed in the following list of general principles:

1. First, in certain embodiments, sabot discarding resistance is reducedor virtually eliminated by adapting the sabot means and the subcaliberprojectile in such a manner that, while engaged together as a functionalunit during some or all of certain stages of the loading and launchingsequence, such as, for example, while being loaded or inserted into thebore, while being held loaded in a predetermined battery dispositionwithin the bore prior to launching, or while undergoing launchacceleration through the bore, the sabot means and the subcaliberprojectile have little or no direct positive connection to each other,but rather have a direct connection which may be essentiallycharacterized as a direct abutting connection or direct abuttinglynesting connection, with some portion of the subcaliber projectileabuttingly engaged rearwardly by some portion of the sabot means. Insuch embodiments, the essential lack of positive connection between thesabot means and the subcaliber projectile provides negligible or noresistance to axial displacement of the subcaliber projectile forwardlyrelative the sabot means, nor to axial displacement of the sabot meansrearwardly relative the subcaliber projectile. Therefore, in many suchembodiments, the sabot means and the subcaliber projectile aremaintained in connection as a functional unit, which functional unit wemay refer to as the sabot projectile assembly, during some or all ofcertain stages of the loading and launching sequence by being externallyurged, biased, or confined against each other by one or more externalconnecting or restraining means, such as one or more detent means. Inmany such embodiments, the external connecting or restraining means alsoserves to prevent any premature axial displacement of the sabotprojectile assembly relative the barrel bore after loading insertion andprior to commencement of launch acceleration. The abutting or nestinglyabutting connection between the sabot means and the subcaliberprojectile, as described above, enables them, once they have exited thebarrel bore and are thus removed from the influence of any detent meansor any other type of connecting means, are also clear of frictionalengagement with the barrel bore, and are furthermore no longer securedtogether by acceleration of the sabot means against the inertial mass ofthe subcaliber projectile, to separate very cleanly and quickly withminimal or virtually no transmission of drag, impulse, torque, or otherpertubations from the sabot means to the subcaliber projectile duringthe discarding process.

2. Second, in certain embodiments, launching resistance is reduced orminimized by adapting the external connecting means, restraining means,detent means or any other means used to prevent premature axialdisplacement of the sabot projectile assembly as mentioned above, insuch a manner so as to impose an initial launching resistance readilyovercome by the pressure differential established upon the sabotprojectile assembly by the user's breath during launch. Different typesof such external connecting means, which, according to the particularembodiment, may be employed either individually or in variouscombinations, include, but are not limited to: one or more associatedmagnetic detent means, one or more electromagnetic detent means, one ormore mechanical detent means, as well as, or alternatively, gravity,inertia, mild frictional engagement with the barrel bore, mildforce-fit, suction, and the manual grip of the user. When used incombination in certain embodiments, such detent means or otherconnecting means may, for example, function antagonistically to pressthe sabot means against the subcaliber projectile, or to confine thesabot means and subcaliber projectile either against each other orwithin a predetermined proximity to one another. Generally speaking, incertain, though not all, embodiments of my invention, the externalconnecting means or detent means, although it might be considered as atype of positive connecting means, is not an integral component or setof components of the sabot projectile assembly, and therefore does notundergo launch acceleration or discarding, but rather is usually affixedto or integral with the blow-gun barrel or mouthpiece or both, and isreused from shot to shot.

3. Third, in certain embodiments, launching resistance is further keptto a minimum by utilizing a sabot means which, after the initiallaunching resistance described above has been overcome, is able totravel down a given bore with as little, or even less, resistance thanthe piston means of a typical full caliber blowgun projectile sized andshaped to fit the same bore. Certain embodiments of my invention mayindeed make this possible, being able to efficiently utilize a sabotmeans shaped and sized so that the amount of surface area contact andsnugness of fit between the sabot and the bore is essentially equal toor even somewhat less than that of the fixed piston means of a fullcaliber projectile sized to fit the same sized bore. It should be notedthat many full caliber blowgun projectiles, although dimensioned to fitthe bore somewhat loosely, still tend to be fitted snugly enough toprevent them sliding too easily down the bore before launch, due togravitational urging when the barrel is tilted away from a horizontallevel, or due to normal movement and reorientation of the barrel duringcarrying and handling the blowgun. Even so, the user of many types ofprior art blowguns must be careful not to tilt the barrel too abruptlyor insert the projectile too forcefully, or else the projectile mayslide partially or completely down the barrel before launch. Certainembodiments of my invention correct this situation in one or more ways.First, the detent means or other means employed to prevent prematureaxial displacement of the sabot projectile assembly components may be soadapted as to hold the projectile assembly sufficiently strongly toprevent premature axial displacement of the sabot projectile assemblycomponents due to gravitational urging, jolts, jars, or swinging of thebarrel, and so forth. In some embodiments, therefore, the user can eventilt the barrel vertically with the muzzle down, without dislodging ordisplacing the sabot projectile assembly from its secure loadedpositioning, which is preferably at or near the breech. Some of suchembodiments that use the detent means or other means to preventpremature axial displacement of either a sabot projectile assembly, oreven of a full caliber projectile, may also provide one or more of thefollowing benefits:

a. The fit of the piston or sabot means within the bore may, if desired,be made slightly looser, since secure frictional engagement between thesabot means and the bore is no longer necessary to prevent prematureaxial displacement of the projectile or projectile assembly. Theslightly looser fit of the piston or sabot means in the bore may resultin a reduction in total remaining launching resistance after the initiallaunching resistance is overcome.

b. The loaded positioning and loaded orientation of the sabot projectileassembly may in certain embodiments be made very consistent andrepeatable with each shot, yielding improved shot-to-shot accuracy.

c. As launch thrust commences, the initial launching resistance, imposedby the detent means or other means of preventing premature axialdisplacement of the projectile or projectile assembly, may cause a delayin the movement of the projectile or projectile assembly. This delay,although usually so slight or short in duration as to be virtuallyundetectable by the user, nevertheless may allow higher launch pressuresto develop, or at least allow pressures to develop to a given level atearlier stages of the projectile's or projectile assembly's travel alongthe bore during launch. The additional thrust generated by the higherlaunch pressures, or earlier peak in pressures, may help to offset theslight delay caused by the initial launching resistance, and in fact mayresult in increased exit velocity of the projectile or projectileassembly. This effect may be amplified by using a piston or sabot meanswith a slightly looser fit as described above, in which case the higherlaunch pressures developed may also help to offset the slightly reducedlateral area of the looser fitting piston or sabot means, therebypossibly avoiding any substantial reduction in thrust and in someembodiments possibly actually yielding increased thrust.

Note: It may be understood that premature or excessive transversedisplacement of the sabot means and subcaliber projectile relative eachother before and during launch acceleration may be substantiallyprevented by any nesting relationship or loosely penetrativerelationship in their connection, or alternatively by the transversetravel limits imposed by the cross-sectional dimensions of the barrelbore.

As was mentioned above, in general, in certain embodiments of myinvention, the external connecting means or restraining means or detentmeans, although it might be considered as a type of positive connectingmeans, is not an integral component or set of components of the sabotprojectile assembly, and therefore does not undergo launch accelerationor discarding, but rather is usually affixed to or integral with theblowgun barrel or mouthpiece or both, and is reused from shot to shot.Other embodiments of my invention, do, however, utilize means forproviding a positive connection between the subcaliber projectile andthe sabot means, in which the positive connecting means may beconsidered as actually being an integral component or set of componentsof the sabot projectile assembly, and as such, in some embodiments mayalso undergo launch acceleration or discarding. The option to use suchintegral positive connecting means provides a wider range ofresponsiveness to user preference or convenience in storing, carrying,handling, and loading the sabot projectile assembly. In cooperation withsuch integral positive connecting means, some embodiments of myinvention may also employ a means of providing an additional oralternative source of force or impulse, in addition to or in place ofatmospheric drag, to actuate sabot disengagement and discarding. Someembodiments may employ a positive connection or positive connectingmeans which is manually disengageable prior to or during loading.Additional information about certain embodiments which utilize integralor affixed positive connecting means between the projectile and thesabot will be provided in later sections. Various advantages, methods ofuse, and alternate embodiments will also be listed or described in latersections.

It should also be noted that in some embodiments of my invention, it maynot be necessary for the subcaliber projectile and the sabot means to bein direct contact or connection with each other during all stages of theloading and launching sequence. In some embodiments, the subcaliberprojectile and sabot means may be loaded sequentially rather thansimultaneously, and additionally or alternatively, rather than beingdirectly abutting while in loaded position within the bore prior launchacceleration, the subcaliber projectile and sabot means may simply besecured or confined within reasonable proximity of one another, so thatthey may assume an abutting relationship once launch accelerationcommences. Furthermore, in some embodiments it may not be necessary forthe sabot means, after being loaded, and before launch acceleration, tobe in direct contact or actual engagement with the sabot detent, inwhich case the sabot detent may simply serve to ensure that the sabotmeans does not exit back out the breech or does not undergo axialdisplacement past a certain predetermined distance from the subcaliberprojectile after loading insertion has been completed and before launchacceleration commences. In some embodiments similar qualifications mayapply to the projectile and projectile detent.

The ability to launch subcaliber projectiles efficiently and accuratelyfrom a blow-gun is a major strategy for improving blowgun performanceset forth by this disclosure. However, this disclosure also sets forthseveral other strategies for improving blowgun performance which may beused complementarily with the strategy of launching subcaliberprojectiles, and which allow the user to exploit the ability to launchsubcaliber projectiles to achieve complementary or related improvementsin areas such as internal ballistic stability as the projectile orprojectile assembly is accelerated through the bore, as well asimprovement in methods of target shooting. Several of thesecomplementary strategies may also be used on their own, independently ofthe strategy of launching subcaliber projectiles, in order to providestand-alone solutions for improving blowgun performance even when usingfull-caliber projectiles rather than subcaliber projectiles. Indeed, myinvention achieves its functions and advantages through strategies orprinciples that operate independently of, and yet in certain embodimentscompatibly with, prior-art blowgun embodiments. Thus, in addition tobeing used to provide a complete set including a blowgun with associatedsabot projectiles, as was described in the brief outline above, alongwith, if so desired, an associated target particularly suited for usewith the blowgun and projectiles, as will be described below, myinvention may alternatively be used to provide stand-alone solutionssuch as projectiles, sabots, kits, accessories, and targets that wouldallow a user, for example, to convert a pre-existing blowgun to launchsubcaliber projectiles, or to build or assemble from scratch his or herown subcaliber blowgun, or to use pre-existing or other full caliberprojectiles as subcaliber projectiles in a blowgun of larger caliber,or, for example, to allow resupply, repair, and maintenance of thecomplete set described above, or of any of the accessory kits orconverter kits or stand-alone solutions suggested above. It isaccordingly desired that protection be provided to such stand-alonesolution embodiments as well as to embodiments that provide a completeset such as the blowgun with associated sabot projectiles described inthe outline above. Other stand-alone solutions include embodiments suchas the improved type of full caliber projectiles which comprise anelongate subcaliber projectile converted into a full caliber projectileby essentially permantly affixing a full caliber piston to the otherwisesubcaliber projectile, as was described above. Another example of astand-alone solution provided by the principles of my invention, anddescribed and illustrated earlier, is a blowgun barrel bore providedwith one or more substantially straight longitudinal bore grooves(or/and in certain embodiments straight longitudinal bore protrusions)in order to thereby provide enhanced internal ballistic guidance to theforward end or other cooperating portion of either a sabot projectileassembly or a full caliber projectile, thus providing enhanced internalballistic stability to either an appropriately adapted subcaliberprojectile or an appropriately adapted full caliber projectile,depending on the particular embodiment and particular method of use. Inturn, such improved internal ballistic guidance and internal ballisticstability of the projectile may yield improved external ballisticstability and accuracy of the projectile. Due to the performanceadvantages of such a straight-grooved barrel bore in terms of providingimproved projectile guidance, stability, and accuracy, and the abilityto selectably use such a straight-grooved barrel bore with either fullcaliber (fixed piston) projectiles or subcaliber (discarding piston)projectiles, it is desired that protection be provided to this area (thestraight-grooved barrel bore) whether used in conjunction with otherfeatures of my invention or used as a stand alone solution, as is truealso for the use of other features of my invention either conjointly orindividually in complete sets, in partial sets, or in stand-aloneapplications.

I claim:
 1. An apparatus for launching subcaliber projectiles,comprising: a blowgun means, said blowgun means including an elongatebarrel provided with a substantially straight bore communicating betweena breech opening and a muzzle opening; a sabot means sized, shaped andadapted for launch through and out said bore by the breath of the user,said sabot means including firstly a rearward facingthrust-pressurization surface adapted to receive thrust pressuresupplied by the breath of the user and thereby be accelerated duringlaunch and secondly a projectile-engaging sabot registration means, saidsabot registration means including a forward facing thrust-transmittingsurface and a forwardly extending projectile-alignment stop meansdisposed in proximity of said thrust-transmitting surface; and asubcaliber projectile means sized, shaped, and adapted for launchthrough and out said bore by thrust transmitted by abutting engagementwith said sabot means, said subcaliber projectile means including arearward facing thrust-receiving surface adapted to abuttingly engagesaid thrust-transmitting surface of said sabot means in such manner thatsaid sabot means may thereby efficiently transmit thrust to saidsubcaliber projectile means during launch acceleration and separate fromsaid subcaliber projectile means after launch acceleration; wherein:said sabot means and said subcaliber projectile means are adapted toexit said muzzle opening after launch acceleration; wherein: said sabotmeans is adapted in such manner that, after launch acceleration,atmospheric drag upon said sabot means may cause said sabot means toseparate from and discard from said subcaliber projectile means;wherein: said projectile-alignment stop means is sized, shaped, andadapted in such manner that, when said thrust-receiving surface isabuttingly engaged with said thrust-transmitting surface, at least onesurface portion of said projectile-alignment stop means is disposedalongside at least one surface portion of said subcaliber projectilemeans, whereby said projectile-alignment stop means is configured toabuttingly stop said subcaliber projectile means from excessive lateraldisplacement and to thereby maintain said sabot means in registrationwith said subcaliber projectile means; and wherein: said sabot means andsaid subcaliber projectile means are cooperatively adapted to beconfigurable with each other in such manner that, when said subcaliberprojectile means and said sabot means are located fully insertedtogether within said bore with said thrust-transmitting surfaceabuttingly engaged with said thrust-receiving surface, at least oneportion of said subcaliber projectile means may touch the inner surfaceof said bore.
 2. The apparatus of claim 1, wherein said subcaliberprojectile means includes an elongate penetrator rod portion; andwherein: said sabot means and said subcaliber projectile means areadapted to be configurable together within said bore, in readiness forlaunching, in such manner that at least one portion of said elongatepenetrator rod portion may, pending commencement of launch acceleration,touch the inner surface of said bore.
 3. The apparatus of claim 1,wherein said subcaliber projectile means further includes a magneticallyattractable portion, and wherein said blowgun means further includes adetent means, said detent means including a magnetic means adapted toproduce a magnetic field, with said magnetic means disposed and orientedin such manner that said magnetically attractable portion of saidsubcaliber projectile means may be brought within influence of saidmagnetic field when said subcaliber projectile means and said sabotmeans are fully inserted together within said bore in readiness forlaunching, whereby said magnetic means may, pending commencement oflaunch acceleration, exert a magnetic restraining influence upon saidmagnetically attractable portion and thereby magnetically engage andhold said subcaliber projectile means in proximity of said sabot means;and wherein: said magnetic means is adapted in such manner that thepressure of the user's breath received into said bore may establish apressure differential across said sabot means sufficient to release saidsubcaliber projectile means from the said magnetic restraining influenceof said magnetic means as launch acceleration commences.
 4. Theapparatus of claim 1, wherein said sabot means comprises a conical shellportion.
 5. The apparatus of claim 1, wherein said sabot registrationmeans is adapted to supportingly carry at least one portion of saidsubcaliber projectile means during launch acceleration.
 6. The apparatusof claim 1, wherein said sabot registration means is non-petaling.
 7. Anapparatus for launching subcaliber projectiles, comprising: an elongatebarrel, said barrel including an elongate, substantially straight borecommunicating between a breech opening and a muzzle opening; a sabotmeans, said sabot means being sized, shaped and adapted for launchthrough and out said bore by the breath of the user; a subcaliberprojectile means containing a magnetically attractable portion, saidsubcaliber projectile means being sized, shaped, and adapted for launchthrough and out said bore by thrust transmitted by abutting engagementwith said sabot means; and a detent means, said detent means including amagnetic means adapted to produce a magnetic field, with said magneticmeans disposed in such manner that said magnetically attractable portionof said subcaliber projectile means may be brought within influence ofsaid magnetic field when said subcaliber projectile means and said sabotmeans are fully inserted together within said bore in readiness forlaunching, whereby said magnetic means may exert a magnetic restraininginfluence upon said magnetically attractable portion and therebymagnetically engage and hold said subcaliber projectile means withinsaid bore in proximity of said sabot means pending commencement oflaunch acceleration; wherein: said magnetic means is adapted in suchmanner that the pressure of the user's breath received into said boremay establish a pressure differential across said sabot means sufficientto release said subcaliber projectile means from the said magneticrestraining influence of said magnetic means as launch accelerationcommences; wherein: said sabot means is adapted to abuttingly engagesaid subcaliber projectile means in such manner that, during launchacceleration, at least one portion of said subcaliber projectile meansmay touch the inner surface of said bore; wherein: said subcaliberprojectile means is adapted in such manner that said subcaliberprojectile means may separate from said sabot means after launchacceleration and travel in flight unencumbered by said sabot means; andwherein: said sabot means and said subcaliber projectile means areadapted to exit said muzzle opening after launch acceleration.
 8. Theapparatus of claim 7, wherein said subcaliber projectile means includesan elongate penetrator rod portion; and wherein: said sabot means andsaid subcaliber projectile means are adapted to be configurable togetherwithin said bore, in readiness for launching, in such manner that atleast one portion of said elongate penetrator rod portion may, pendingcommencement of launch acceleration, touch the inner surface of saidbore.
 9. The apparatus of claim 8, wherein said subcaliber projectilemeans includes an aerodynamic stabilizer means.
 10. An apparatus forlaunching subcaliber projectiles, comprising: an elongate barrel, saidbarrel including an elongate, substantially straight bore communicatingbetween a breech opening and a muzzle opening; a sabot means, said sabotmeans being sized, shaped and adapted for launch through and out saidbore by the breath of the user; a subcaliber projectile means containinga magnetically attractable portion, said subcaliber projectile meansbeing sized, shaped, and adapted for launch through and out said bore bythrust transmitted by abutting engagement with said sabot means; and adetent means, said detent means including a magnetic means adapted toproduce a magnetic field, with said magnetic means disposed in suchmanner that said magnetically attractable portion of said subcaliberprojectile means may be brought within influence of said magnetic fieldwhen said subcaliber projectile means and said sabot means are fullyinserted together within said bore in readiness for launching, wherebysaid magnetic means may exert a magnetic restraining influence upon saidmagnetically attractable portion and thereby magnetically engage andhold said subcaliber projectile means within said bore in proximity ofsaid sabot means pending commencement of launch acceleration; wherein:said magnetic means is adapted in such manner that the pressure of theuser's breath received into said bore may establish a pressuredifferential across said sabot means sufficient to release saidsubcaliber projectile means from the said magnetic restraining influenceof said magnetic means as launch acceleration commences; wherein: saidsabot means and said subcaliber projectile means are adapted to beconfigurable within said bore, in readiness for launching, in suchmanner that at least one portion of said subcaliber projectile meansmay, pending commencement of launch acceleration, touch the innersurface of said bore; wherein: said sabot means is adapted to separatefrom said subcaliber projectile means, after launch acceleration andthereby permit said subcaliber projectile means to travel in flightunencumbered by said sabot means; and wherein: said sabot means and saidsubcaliber projectile means are adapted to exit said muzzle openingafter launch acceleration.
 11. The apparatus of claim 10, wherein saidsabot means is sized, shaped and adapted for launch through and out saidbore by the breath of the user.
 12. The apparatus of claim 10, whereinsaid subcaliber projectile means includes an elongate penetrator rodportion; and wherein: said sabot means and said subcaliber projectilemeans are adapted to be configurable together within said bore, inreadiness for launching, in such manner that at least one portion ofsaid elongate penetrator rod portion may, pending commencement of launchacceleration, touch the inner surface of said bore.
 13. An apparatus forlaunching subcaliber projectiles from a blowgun, comprising: a sabotmeans sized, shaped and adapted for launch through and out the bore of ablowgun by the breath of the user, said sabot means including firstly arearward facing thrust-pressurization surface adapted to receive thrustpressure supplied by the breath of the user and thereby be acceleratedduring launch and secondly a projectile-engaging sabot registrationmeans, said sabot registration means including a forward facingthrust-transmitting surface and a forwardly extendingprojectile-alignment stop means disposed in proximity of saidthrust-transmitting surface; wherein: said sabot means is adapted toexit the bore of the blowgun after launch acceleration; wherein: saidthrust-transmitting surface of said sabot means is adapted to abuttinglyengage a subcaliber blowgun projectile in such manner that said sabotmeans may thereby efficiently transmit thrust to the subcaliber blowgunprojectile during launch and separate from the subcaliber blowgunprojectile after launch acceleration; wherein: said projectile-alignmentstop means is sized, shaped, and adapted in such manner that, when saidthrust-transmitting surface is abuttingly engaged with the subcaliberblowgun projectile in readiness for launch, at least one surface portionof said projectile-alignment stop means is disposed alongside at leastone surface portion of the subcaliber blowgun projectile, whereby saidprojectile-alignment stop means is configured to abuttingly stop thesubcaliber blowgun projectile from excessive lateral displacement and tothereby maintain said sabot means in registration with the subcaliberblowgun projectile; and wherein: said sabot means is adapted to beconfigurable with the subcaliber blowgun projectile in such manner that,when the subcaliber blowgun projectile and said sabot means are fullyinserted together within the barrel bore of the blowgun with said sabotmeans abuttingly engaged in registration with the subcaliber blowgunprojectile, at least one portion of the subcaliber blowgun projectilemay touch the inner surface of the barrel bore of the blowgun.
 14. Theapparatus of claim 13, in which said sabot means comprises a conicalshell portion.
 15. The apparatus of claim 13, wherein said sabotregistration means is adapted in such manner that, when saidthrust-transmitting surface is abuttingly engaged with the subcaliberblowgun projectile during launch acceleration, said sabot registrationmeans may supportingly carry at least one portion of the subcaliberblowgun projectile during launch acceleration.
 16. The apparatus ofclaim 15, in which said sabot registration means is non-petaling.
 17. Acombined blowgun and sabot projectile means, comprising: a blowgun, saidblowgun including an elongate barrel provided with an elongate,substantially straight bore communicating between a breech opening and amuzzle opening, and a sabot projectile means, said sabot projectilemeans including a sabot projectile adapted for launch through and outsaid bore by thrust supplied by the breath of the user, said sabotprojectile containing a sabot means and a subcaliber projectile means,with said subcaliber projectile means containing at least one subcaliberprojectile, with said sabot means containing a forward-facing surfaceadapted to abuttingly engage a rearward-facing surface of saidsubcaliber projectile means in such a manner that said sabot means maythereby efficiently transmit thrust to said subcaliber projectile meansduring launch, yet also in such a manner that said sabot means mayseparate from and discard from said subcaliber projectile means at theconclusion of launch acceleration.
 18. The apparatus of claim 17,wherein said sabot means comprises a conical shell portion.
 19. Theapparatus of claim 17, wherein said sabot means is non-petaling.